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 31988U 99025CPR 25263.43518637 .00004311 00000-0 20217-2 0 9992
2 31988 98.1423 339.3658 0064107 172.8059 187.4054 14.19504315629701
| Epoch (UTC): | 20 September 2025 10:26:40 |
| Eccentricity: | 0.0064107 |
| inclination: | 98.1423° |
| perigee height: | 781 km |
| apogee height: | 873 km |
| right ascension of ascending node: | 339.3658° |
| argument of perigee: | 172.8059° |
| revolutions per day: | 14.19504315 |
| mean anomaly at epoch: | 187.4054° |
| orbit number at epoch: | 62970 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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