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 21797U 91081B 25196.97387977 .00000114 00000-0 97261-4 0 9990
2 21797 82.9522 30.2232 0039305 98.8755 11.9264 13.77822217690389
| Epoch (UTC): | 15 July 2025 23:22:23 |
| Eccentricity: | 0.0039305 |
| inclination: | 82.9522° |
| perigee height: | 943 km |
| apogee height: | 1000 km |
| right ascension of ascending node: | 30.2232° |
| argument of perigee: | 98.8755° |
| revolutions per day: | 13.77822217 |
| mean anomaly at epoch: | 11.9264° |
| orbit number at epoch: | 69038 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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