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 9904U 77024B 22146.81513645 -.00000040 00000-0 -30670-4 0 9996
2 9904 81.2624 186.0071 0052748 285.6910 73.8444 14.06937562316549
| Epoch (UTC): | 26 May 2022 19:33:47 |
| Eccentricity: | 0.0052748 |
| inclination: | 81.2624° |
| perigee height: | 831 km |
| apogee height: | 908 km |
| right ascension of ascending node: | 186.0071° |
| argument of perigee: | 285.6910° |
| revolutions per day: | 14.06937562 |
| mean anomaly at epoch: | 73.8444° |
| orbit number at epoch: | 31654 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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