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 16631U 86014H 25197.49596169 .00007063 00000-0 41174-3 0 9995
2 16631 63.2908 252.0267 0796920 105.9595 263.0669 13.84956984297735
| Epoch (UTC): | 16 July 2025 11:54:11 |
| Eccentricity: | 0.0796920 |
| inclination: | 63.2908° |
| perigee height: | 362 km |
| apogee height: | 1530 km |
| right ascension of ascending node: | 252.0267° |
| argument of perigee: | 105.9595° |
| revolutions per day: | 13.84956984 |
| mean anomaly at epoch: | 263.0669° |
| orbit number at epoch: | 29773 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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