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 10577U 77121U 22222.70954326 .00000050 00000-0 14139-3 0 9990
2 10577 65.7941 196.6280 0145023 266.3217 270.3703 13.68212788225320
| Epoch (UTC): | 10 August 2022 17:01:44 |
| Eccentricity: | 0.0145023 |
| inclination: | 65.7941° |
| perigee height: | 899 km |
| apogee height: | 1113 km |
| right ascension of ascending node: | 196.6280° |
| argument of perigee: | 266.3217° |
| revolutions per day: | 13.68212788 |
| mean anomaly at epoch: | 270.3703° |
| orbit number at epoch: | 22532 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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