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 09904U 77024B 22145.60616767 -.00000046 00000-0 -34246-4 0 9990
2 09904 81.2627 187.1750 0052861 289.1556 70.3896 14.06937750316147
| Epoch (UTC): | 25 May 2022 14:32:52 |
| Eccentricity: | 0.0052861 |
| inclination: | 81.2627° |
| perigee height: | 831 km |
| apogee height: | 908 km |
| right ascension of ascending node: | 187.1750° |
| argument of perigee: | 289.1556° |
| revolutions per day: | 14.06937750 |
| mean anomaly at epoch: | 70.3896° |
| orbit number at epoch: | 31614 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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