View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 31793U 07029B 25197.55160242 .00000163 00000-0 10947-3 0 9994
2 31793 70.9775 308.7434 0002281 281.6041 93.3808 14.14792295932069
| Epoch (UTC): | 16 July 2025 13:14:18 |
| Eccentricity: | 0.0002281 |
| inclination: | 70.9775° |
| perigee height: | 841 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 308.7434° |
| argument of perigee: | 281.6041° |
| revolutions per day: | 14.14792295 |
| mean anomaly at epoch: | 93.3808° |
| orbit number at epoch: | 93206 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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