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 38735U 12041C 25343.82874234 .00000025 00000-0 10835-3 0 9996
2 38735 82.4758 192.7533 0017840 119.3069 240.9796 12.42640344606325
| Epoch (UTC): | 09 December 2025 19:53:23 |
| Eccentricity: | 0.0017840 |
| inclination: | 82.4758° |
| perigee height: | 1481 km |
| apogee height: | 1509 km |
| right ascension of ascending node: | 192.7533° |
| argument of perigee: | 119.3069° |
| revolutions per day: | 12.42640344 |
| mean anomaly at epoch: | 240.9796° |
| orbit number at epoch: | 60632 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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