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 28075U 99057NF 22222.27184739 .00000671 00000-0 22120-3 0 9997
2 28075 98.7841 239.6783 0104569 62.7369 298.4422 14.38433689531590
| Epoch (UTC): | 10 August 2022 06:31:27 |
| Eccentricity: | 0.0104569 |
| inclination: | 98.7841° |
| perigee height: | 689 km |
| apogee height: | 838 km |
| right ascension of ascending node: | 239.6783° |
| argument of perigee: | 62.7369° |
| revolutions per day: | 14.38433689 |
| mean anomaly at epoch: | 298.4422° |
| orbit number at epoch: | 53159 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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