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 25193.69282156 .00000112 00000-0 95327-4 0 9998
2 21797 82.9521 32.6627 0039253 107.7351 297.6963 13.77821459689931
| Epoch (UTC): | 12 July 2025 16:37:39 |
| Eccentricity: | 0.0039253 |
| inclination: | 82.9521° |
| perigee height: | 943 km |
| apogee height: | 1000 km |
| right ascension of ascending node: | 32.6627° |
| argument of perigee: | 107.7351° |
| revolutions per day: | 13.77821459 |
| mean anomaly at epoch: | 297.6963° |
| orbit number at epoch: | 68993 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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