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 22139.84579636 -.00000010 00000-0 -13008-4 0 9996
2 09904 81.2641 192.7408 0053110 305.5589 54.0635 14.06938491315335
| Epoch (UTC): | 19 May 2022 20:17:56 |
| Eccentricity: | 0.0053110 |
| inclination: | 81.2641° |
| perigee height: | 831 km |
| apogee height: | 908 km |
| right ascension of ascending node: | 192.7408° |
| argument of perigee: | 305.5589° |
| revolutions per day: | 14.06938491 |
| mean anomaly at epoch: | 54.0635° |
| orbit number at epoch: | 31533 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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