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 31906U 99025CLH 24357.85809483 .00009035 00000-0 42152-2 0 9993
2 31906 98.6778 130.0086 0051807 73.4805 77.8999 14.19888761900834
| Epoch (UTC): | 22 December 2024 20:35:39 |
| Eccentricity: | 0.0051807 |
| inclination: | 98.6778° |
| perigee height: | 788 km |
| apogee height: | 863 km |
| right ascension of ascending node: | 130.0086° |
| argument of perigee: | 73.4805° |
| revolutions per day: | 14.19888761 |
| mean anomaly at epoch: | 77.8999° |
| orbit number at epoch: | 90083 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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