Simulation of Access, Coverage, and Orbital Decay for an Optical Micro-Satellite for Colombia*

Simulación del acceso, la cobertura y la decadencia orbital de un microsatélite óptico para Colombia

Ernesto David Cortés García , Germán Darío Saenz Hernández , Lorena Paola Cárdenas Espinosa , Santiago Muñoz Giraldo , Dib Ziyari Salek Chaves , Rubén Darío Guerrero Sánchez

Simulation of Access, Coverage, and Orbital Decay for an Optical Micro-Satellite for Colombia*

Ingeniería y Universidad, vol. 29, 2025

Pontificia Universidad Javeriana

Ernesto David Cortés García

Colombian Air Force, Colombia


Germán Darío Saenz Hernández

Colombian Air Force, Colombia


Lorena Paola Cárdenas Espinosa

Colombian Air Force, Colombia


Santiago Muñoz Giraldo a

Colombian Air Force, Colombia


Dib Ziyari Salek Chaves

Colombian Air Force, Colombia


Rubén Darío Guerrero Sánchez

Colombian Air Force, Colombia


Received: 28 october 2024

Accepted: 29 august 2025

Published: 29 september 2025

Abstract: The selection of the operational orbit is a critical component for the success of satellite missions, as it must meet specific user requirements, payload constraints, and communication needs. This paper comprehensively analyzes the criteria and parameters used to determine the best orbit for satellite missions, focusing on design variables derived from mission requirements and technical constraints. Several fundamental aspects are evaluated, including coverage of areas of interest, access times to ground stations, revisit times, and satellite lifespan in orbit, through simulations of orbital scenarios. The results show that orbits with inclinations of 16° provide an optimal balance between coverage and revisit times, maximizing operational efficiency over Colombian territory. Satellite constellations are also analyzed, highlighting specific combinations that improve coverage and access times. Furthermore, the analysis of orbital decay and lifespan in orbit confirms that the selected orbits comply with international standards for mitigating collision risk. This article offers a guide for orbit selection in satellite missions, emphasizing a Low-Earth Orbit (LEO) mission, ensuring operational benefits and minimizing risks.

Keywords:Satellite Orbits, Coverage, Revisit Time, Orbit Lifespan, Simulation, Decay, Microsatellite.

Resumen: La selección de una órbita operacional es un factor crítico para el éxito de las misiones satelitales, ya que debe cumplir con requisitos específicos del usuario, restricciones de carga útil y necesidades de comunicación. Este artículo presenta un análisis exhaustivo de los criterios y parámetros utilizados para determinar la órbita óptima para misiones satelitales, enfocándose en variables de diseño derivadas de los requisitos de la misión y restricciones técnicas. Se evalúan aspectos clave, como la cobertura de áreas de interés, los tiempos de acceso a estaciones terrestres, los tiempos de revisita y la vida útil del satélite en órbita, a través de simulaciones de escenarios orbitales. Los resultados indican que las órbitas con inclinaciones de 16° proporcionan un equilibrio óptimo entre cobertura y tiempos de revisita, maximizando la eficiencia operacional sobre el territorio colombiano. El estudio también examina constelaciones de satélites, destacando configuraciones específicas que mejoran la cobertura y los tiempos de acceso. Además, el análisis de la desintegración orbital y la vida útil en órbita confirma que las órbitas seleccionadas cumplen con los estándares internacionales de mitigación de riesgos de colisión. Este artículo sirve como guía para la selección de órbitas en misiones satelitales, con énfasis en misiones en órbitas bajas, asegurando beneficios operacionales y minimizando riesgos.

Palabras clave: órbitas satelitales, cobertura, tiempos de revisita, vida útil en órbita, simulación, decaimiento, microsatélite.

Introduction

The space industry has experienced significant growth in recent decades, driven by the development of advanced technologies and the increasing demand for satellite services. This has encouraged emerging countries to develop their capabilities in the space sector, starting from mission design to in-depth analysis [1]. In this context, orbit selection for satellite missions has become a critical factor in maximizing operational efficiency and ensuring mission success. The proper selection of orbit must consider various factors, including coverage of areas of interest, access times to ground stations, revisit times, and the satellite’s orbital lifespan [2].

In the case of Colombia, the Colombian Airspace Force (FAC) has led significant advances in the space domain with the launch of the FACSAT-1 satellite and the co-development of the FACSAT-2 “Chiribiquete” satellite mission. These assets have contributed to the development of capabilities, including data collection from Earth Observation sensors, autonomous satellite operation, as well as capability enhancement in mission design, software development, payload operation, and data analysis applications. These foundations have set the stage for future mission developments in the country.

FACSAT-1, launched in 2018, was the country’s first Earth observation satellite, which enabled the autonomous operation of an optical data acquisition system. FACSAT-2, its successor, has improved payload and communication capabilities. The primary payload acquires multispectral images, while a secondary payload collects spectral signatures. These data are used for developments such as deforestation analyses and Greenhouse Gas (GHG) emission monitoring [3] [4].

Currently, a new satellite mission is under analysis, building on the achievements of its predecessors and incorporating technological advancements and lessons learned to optimize performance. This article focuses on the orbit selection for a future satellite mission by analyzing parameters and criteria that ensure a balance between coverage, access times, revisit times, and orbital lifespan, to maximize return on investment. Through simulations and evaluations of different orbital scenarios, this research seeks to identify the best configuration to meet the objectives of a new Earth observation mission with enhanced capabilities to address the country’s needs.

To achieve this, a detailed analysis of orbital variables is presented, evaluating inclined orbits and sun-synchronous orbits (SSO) to determine which offers the best balance between coverage and operational efficiency. The results of this research provide a guide for orbit selection in future satellite missions, contributing to the ongoing development of Colombia’s space capabilities.

Materials and Methods: Mission and Requirements

Figure 1 presents the methodology developed to select the most suitable orbit by transforming mission requirements, payload constraints, and communication requirements into design variables, thereby establishing the orbital parameters for selection [5].

Methodology for Orbital Selection
Figure 1
Methodology for Orbital Selection


Source: Authors.

The choice of the operational orbit for an Earth observation satellite mission is determined by user requirements, as these guide the design and development of systems that must operate reliably under extreme conditions [6]. Table 1 presents the main mission requirements, including the constraints provided by the payload and communications systems. [5].

Among the mission requirements, some of the most relevant aspects include: the type of orbit and altitude, which determine the range of latitudes available for the satellite to cover; the area of interest; the number of accesses; and the revisit times, which determine what regions on Earth can be studied and how they can be accessed. Lastly, the orbital lifespan refers to how long the satellite can remain in orbit while operating nominally.

Within the payload constraints, the Off-Nadir angle is particularly noteworthy, as it defines the maximum inclination a satellite can achieve from the nadir side while maintaining effective imaging capabilities [7]. The operational time refers to the optimal period during which a sensor can effectively capture data, considering environmental conditions and the orbital trajectory [8].

Finally, among the communication constraints, the elevation angle stands out as a limitation caused by Colombia’s mountainous terrain. The minimum access time determines the efficiency of the link between satellites and ground stations, which affects the quality of communication services. [9] [10].

Table 1
Mission Requirements and Constraints
 Mission Requirements and Constraints


Source: Authors.

The criteria outlined in Table 1 are the primary focus for simulating scenarios, allowing the identification of the best orbital aspects that benefit the satellite mission. The aim is to find a way to address and satisfy these requirements [11].

Table 2 lists the design variables and orbital parameters determined from the mission requirements and constraints. These primarily correspond to the type of orbit, the altitude, the inclination, the eccentricity-perigee argument, the RAAN (Right Ascension of Ascending Node), the sensor, the Off-Nadir angle, the revisit time, and the elevation angle.

Table 2
Effects of Design Variables and Orbital Parameters on Selection Criteria
Effects of Design
Variables and Orbital Parameters on Selection Criteria


Source: Authors.

The variables and parameters have been selected based on their impact on factors of interest for the mission [10], including coverage, orbital lifespan, image resolution, eclipse times, and communication times, among others. The selection criteria arising from the analysis of these factors provide the necessary parameters for simulating various orbital scenarios. Consequently, there will be a specific number of possibilities for the scenarios, and the results will subsequently be analyzed and compared against the selection criteria to identify an orbit with the most favorable aspects for the satellite mission [12].

Results

Design and Simulation (Scenarios)

Based on the selection criteria, three main variables are identified for running the simulations and defining the criteria.

  1. Coverage of the Region: to analyze the coverage of the area of interest.

  2. Access Times to Ground Stations: to analyze the link times between ground stations and the satellite

  3. Orbital Decay: to analyze the satellite’s orbital lifespan [13]

The next simulations are focused on each criterion described. To complement each scenario, some simulation parameters must be defined. Table 3 summarizes these elements:

Table 3
General Aspects of the Simulation Scenarios
General Aspects of the Simulation
Scenarios


Source: Authors.

In the following paragraphs, the results obtained from each simulation will be briefly presented:

Coverage

This simulation utilizes a defined “rectangular” region to include territories that are not part of the continental section of Colombia, such as the islands, allowing for a comprehensive analysis of its territory.

Orbital Plane 10°

Nadir: In general, Figure 2 shows the coverage of a LEO satellite with an inclination of 10° over one year of simulation. The figure illustrates the number of passes over Colombian territory in the Nadir operation.

Number of Passes
for 10° Orbit in Nadir
Figure 2
Number of Passes for 10° Orbit in Nadir


Source: Authors.

The defined region would receive about 12 passes annually, corresponding to an average frequency of one pass per month. The figure depicts a purple area that represents a region of zero coverage, encompassing Barranquilla, La Jagua, and San Andrés. This limitation would prevent meeting the requirement for complete coverage over Colombia. The area with the highest revisit rate would be at the border of the zero-coverage region, as it represents the perigee/apogee of the orbit.

Oblique: Figure 3 illustrates the coverage simulation, showing the number of passes during the Offset operation

Number of Passes for 10° Orbit in Oblique
(Offset)
Figure 3
Number of Passes for 10° Orbit in Oblique (Offset)


Source: Authors.

By Figure 3, an expansion in the coverage area is observed. However, Barranquilla, La Jagua, and San Andrés remain part of the zero-coverage region. Similarly, the number of passes over the Colombian territory increases, with an average of 135 passes per year (11.25 passes per month).

Orbital plane 16°

Nadir. Figure 4 illustrates the coverage simulation, showing the number of passes during Nadir operation.

Number of Passes for 16° Orbit in Nadir
Figure 4
Number of Passes for 16° Orbit in Nadir


Source: Authors.

The defined region would have an average of 10 total passes (2 passes per month). There is a region of zero coverage within the defined area, but it is not part of Colombia. The area with the highest number of passes is outside Colombia. Additionally, it is observed that with this inclination and sensor operation, a complete coverage of the Colombian territory is achieved, ranging from 2 to 14 passes.

Oblique. Figure 5 illustrates the coverage simulation, showing the number of passes during the Offset operation.

Number of Passes for 16° Orbit in Oblique (Offset)
Figure 5
Number of Passes for 16° Orbit in Oblique (Offset)


Source: Authors.

In oblique orientation, as illustrated in Figure 5, a greater degree of uniformity is observed in the annual number of passes over the territory, with values ranging from 77 to 117 passes per year. This includes regions such as Barranquilla, La Jagua, and San Andrés. The results indicate that a portion of the territory is expected to have at least 6.42 passes per month, which is similar to the overall average of 11 passes per month. In this case, the region with the highest number of passes does not belong to Colombia.

Orbital Plane 97°

Nadir: Figure 6 presents the coverage simulation results, detailing the number of passes achieved during Nadir operations.

Number of Passes for 97° Orbit in Nadir
Figure 6
Number of Passes for 97° Orbit in Nadir


Source: Authors.

The defined region would have an average of 2 total passes. Observing Figure 6, a high degree of uniformity is noted, with at least 1 annual pass at each point within the defined region, implying a complete coverage of the area. Certain small regions receive only three passes annually, resulting in an average interval of 121 days between passes.

Oblique: Figure 7 illustrates the coverage simulation, the number of passes during the Offset operation.

Number of Passes for 97° Orbit in Oblique (Offset)
Figure 7
Number of Passes for 97° Orbit in Oblique (Offset)


Source: Authors.

As shown in Figure 7, the coverage area expands into a vertical-diagonal band, receiving 18–23 annual passes. The region averages 20 passes per year, or 1.67 per month.

Communication Access

This simulation uses a 50 km grid, with each node representing a ground station in Colombia. For COLAF, key target points include Cali, Bogotá, Barranquilla, La Jagua, and San Andrés, as they are major cities or strategic sites for building a ground segment facility.

Orbital Plane 16°

Average Access Time (s): Figure 8 illustrates the average access times for a 16° inclined orbit.

Average Access Time for 16° Orbit
Figure 8
Average Access Time for 16° Orbit


Source: Authors.

The average access times in this orbit range from 5.6 to 7.18 minutes, as illustrated in Figure 8. The area with the highest access times is in the north, including BAQ, GUJ, and SPP, while the area with the lowest access times is in the south. The average communication time for the region is approximately 6.58 minutes, while the ground stations in Cali and Bogotá have an average access time of 6.38 minutes.

Maximum Revisit Times (s): Figure 9 illustrates the total revisit times for a 16° inclined orbit.

Total Revisit Times for
16° Orbit
Figure 9
Total Revisit Times for 16° Orbit


Source: Authors.

The longest revisit times are found in the northern area of the defined region, with a minimum of 13 hours. The southern zone achieves the shortest revisit times, with a maximum of 6.69 hours, making it the most favorable area for this orbit. The stations in Cali and Bogotá have a revisit time of 8.36 hours, while Barranquilla and La Jagua have a revisit time of 11.69 hours. On average, the territory has a revisit time of 9.2 hours.

Orbital Plane 97°

Average Access Time (s): Figure 10 illustrates the average access times for a 97° orbit.

Average Access Time for
97° Orbit
Figure 10
Average Access Time for 97° Orbit


Source: Authors.

In this orbit, the average access times are between 5.97 and 6.07 minutes, resulting in a reduced and nearly uniform spectrum across the entire defined region. The Colombian territory has an average access time of approximately 6 minutes, with the ground stations in Cali and Bogotá falling within this average range. The western zone comprises areas with maximum coverage, in which San Andrés is located.

Maximum Revisit Times (s): Figure 11 illustrates the total revisit times for a 97° inclined orbit.

Total Revisit Times for 97° Orbit
Figure 11
Total Revisit Times for 97° Orbit


Source: Authors.

Figure 11 shows the maximum revisit times obtained for this 97° orbit. Where uniformity in revisit times is achieved across the entire Colombian territory, with a duration of 11.83 hours.

Orbital Decay

In this scenario, dimensions sourced from multiple suppliers are used, and the satellites are modeled as rectangular prisms for simulation purposes. Additionally, standard values for the drag coefficient and reflectivity are used, being 2.2 and 1.3, respectively [14] [15] [16]. Table 4 summarizes the results obtained from two simulation software packages: DRAMA and STK.

Table 4
Orbital Decay Results in Years
Orbital Decay Results in
Years


Source: Authors.

In general, it is observed that SSO orbits provide greater longevity compared to orbits near the equator.

Results Analysis

Simulation Results

Coverage Analysis:

Communication Access Analysis:

Orbital Decay:

Results - Selection Criteria

The main criteria selected for the orbit design are the payload constraints, which include resolution, speeds (orbital and satellite) for image capture, offset angle, coverage of the area of interest, and revisit time.

Conclusions: Orbital Selection

After analyzing the previously obtained results, an updated table detailing the orbital requirements for the FACSAT-3 mission is presented below (Table 05):

This table summarizes all the simulations, results, and analyses conducted for the orbital design. This orbit incorporates the requirements for the FACSAT-3 mission and the best aspects for its execution.

Table 0 5
Selected Aspects for the FACSAT-3 Mission Orbit.
 Selected Aspects for the FACSAT-3 Mission Orbit.


Source: Authors.

In conclusion, based on the coverage criteria, link times, orbital lifespan, and compliance with international standards, a 16° inclined orbit with both nadir and oblique (±7.5°) operation represents the best option for Colombia’s optical microsatellite Earth observation mission.

Acknowledgments

To the Colombian Aerospace Force and the Center for Research and Development in Aerospace Technologies (CITAE).

References

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Notes

* Research article

Author notes

aCorresponding author. E-mail: santiago.munoz@fac.mil.co

Additional information

How to cite this article: E D Cortés García, G D Saenz Hernández, L P Cárdenas Espinosa, S Muñoz Giraldo, D Z Salek Chaves, R D Guerrero Sánchez, “Simulation of Access, Coverage, and Orbital Decay for an Optical Micro-Satellite for Colombia” Ing. Univ. vol. 29, 2025. https://doi.org/10.11144/Javeriana.iued29.saco

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