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 28904U 05046C 22222.56690047 .00000082 00000-0 32491-3 0 9997
2 28904 7.4675 313.1947 7195516 300.5584 8.1541 2.29225523139959
| Epoch (UTC): | 10 August 2022 13:36:20 |
| Eccentricity: | 0.7195516 |
| inclination: | 7.4675° |
| perigee height: | 436 km |
| apogee height: | 35402 km |
| right ascension of ascending node: | 313.1947° |
| argument of perigee: | 300.5584° |
| revolutions per day: | 2.29225523 |
| mean anomaly at epoch: | 8.1541° |
| orbit number at epoch: | 13995 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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