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 22144.53943134 -.00000055 00000-0 -39884-4 0 9995
2 9904 81.2629 188.2057 0052889 292.1982 67.3581 14.06937859316224
| Epoch (UTC): | 24 May 2022 12:56:46 |
| Eccentricity: | 0.0052889 |
| inclination: | 81.2629° |
| perigee height: | 831 km |
| apogee height: | 908 km |
| right ascension of ascending node: | 188.2057° |
| argument of perigee: | 292.1982° |
| revolutions per day: | 14.06937859 |
| mean anomaly at epoch: | 67.3581° |
| orbit number at epoch: | 31622 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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