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 22147.81075768 -.00000026 00000-0 -22545-4 0 9992
2 09904 81.2624 185.0449 0052770 282.8584 76.6693 14.06937503316450
| Epoch (UTC): | 27 May 2022 19:27:29 |
| Eccentricity: | 0.0052770 |
| inclination: | 81.2624° |
| perigee height: | 831 km |
| apogee height: | 908 km |
| right ascension of ascending node: | 185.0449° |
| argument of perigee: | 282.8584° |
| revolutions per day: | 14.06937503 |
| mean anomaly at epoch: | 76.6693° |
| orbit number at epoch: | 31645 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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