Coordinate prediction of spacecraft using neural networks

This paper investigates the effectiveness of using neural network models for spacecraft coordinate prediction based on data in TLE (Two-Line Element Set) format. The focus is on comparing the accuracy of trajectory prediction with actual data, where the distance metric between the true and predicted spacecraft trajectories is used to assess quality. Two approaches – neural network prediction and SGP-4 model prediction with consideration of orbital data specificity – are considered. Spacecraft (SC) coordinate prediction is one of the key tasks in space mission control, flight safety and collision avoidance in orbit. With the development of machine learning technologies and neural network methods, it is now possible to consider alternative approaches to SC coordinate prediction. Neural network models can become an effective tool for predicting the coordinates of spacecraft. For successful planning of spacecraft (SC) observations, it is necessary to accurately predict their position and velocity vector in space. The prediction is usually based on the orbital parameters of the spacecraft, represented in TLE (Two-Line Element Set) format. This data, regularly published by NORAD on the platform www.spacetrack.org, is publicly available and is used to calculate the position of satellites. The satellite coordinates and velocity vector are traditionally calculated using the SGP4 (Simplified General Perturbations) model, which serves as the basis for the TLE data. However, studies show that the accuracy of spacecraft coordinate prediction decreases as the time interval between the date of TLE formation and the date of prediction increases. The main reason for this error is a number of simplifications adopted in the motion model and the influence of disturbances that are not fully accounted for in the SGP4 model. The use of more sophisticated physical models may reduce the errors somewhat, but the instabilities in the orbital parameters limit the possibility of significantly improving the forecast accuracy. Nevertheless, assuming that the spacecraft motion is influenced by factors whose statistical parameters are periodic in nature, it is possible to use machine learning techniques such as neural networks for more accurate prediction.

Publication Details

Journal
Achievements of Modern Radioelectronics
Published
2025-05-05
DOI
https://doi.org/10.18127/j20700784-202505-12
Primary Topic
Geochemistry and Geologic Mapping
Type
article
Field-Weighted Citation Impact
0.00
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article

Coordinate prediction of spacecraft using neural networks

Achievements of Modern Radioelectronics
Geochemistry and Geologic Mapping
article

Coordinate prediction of spacecraft using neural networks

article en

Abstract

This paper investigates the effectiveness of using neural network models for spacecraft coordinate prediction based on data in TLE (Two-Line Element Set) format. The focus is on comparing the accuracy of trajectory prediction with actual data, where the distance metric between the true and predicted spacecraft trajectories is used to assess quality. Two approaches – neural network prediction and SGP-4 model prediction with consideration of orbital data specificity – are considered. Spacecraft (SC) coordinate prediction is one of the key tasks in space mission control, flight safety and collision avoidance in orbit. With the development of machine learning technologies and neural network methods, it is now possible to consider alternative approaches to SC coordinate prediction. Neural network models can become an effective tool for predicting the coordinates of spacecraft. For successful planning of spacecraft (SC) observations, it is necessary to accurately predict their position and velocity vector in space. The prediction is usually based on the orbital parameters of the spacecraft, represented in TLE (Two-Line Element Set) format. This data, regularly published by NORAD on the platform www.spacetrack.org, is publicly available and is used to calculate the position of satellites. The satellite coordinates and velocity vector are traditionally calculated using the SGP4 (Simplified General Perturbations) model, which serves as the basis for the TLE data. However, studies show that the accuracy of spacecraft coordinate prediction decreases as the time interval between the date of TLE formation and the date of prediction increases. The main reason for this error is a number of simplifications adopted in the motion model and the influence of disturbances that are not fully accounted for in the SGP4 model. The use of more sophisticated physical models may reduce the errors somewhat, but the instabilities in the orbital parameters limit the possibility of significantly improving the forecast accuracy. Nevertheless, assuming that the spacecraft motion is influenced by factors whose statistical parameters are periodic in nature, it is possible to use machine learning techniques such as neural networks for more accurate prediction.

Achievements of Modern Radioelectronics
Openalex Percentile: Top 70%
Geochemistry and Geologic Mapping
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Coordinate prediction of spacecraft using neural networks · Achievements of Modern Radioelectronics (2025) | TGRS Research Map | TGRS