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 22285U 92093B 23151.93774072 -.00000031 00000-0 82984-5 0 9994
2 22285 71.0223 329.8291 0002956 23.7778 336.3481 14.15155130570181
| Epoch (UTC): | 31 May 2023 22:30:20 |
| Eccentricity: | 0.0002956 |
| inclination: | 71.0223° |
| perigee height: | 839 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 329.8291° |
| argument of perigee: | 23.7778° |
| revolutions per day: | 14.15155130 |
| mean anomaly at epoch: | 336.3481° |
| orbit number at epoch: | 57018 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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