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 21938U 92020B 25194.52363781 .00000100 00000-0 87903-4 0 9994
2 21938 82.9324 331.3802 0027832 244.1532 186.2976 13.75514826668254
| Epoch (UTC): | 13 July 2025 12:34:02 |
| Eccentricity: | 0.0027832 |
| inclination: | 82.9324° |
| perigee height: | 959 km |
| apogee height: | 1000 km |
| right ascension of ascending node: | 331.3802° |
| argument of perigee: | 244.1532° |
| revolutions per day: | 13.75514826 |
| mean anomaly at epoch: | 186.2976° |
| orbit number at epoch: | 66825 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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