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 31807U 99025CGV 22275.88933001 .00001907 00000-0 55204-3 0 9990
2 31807 99.1251 309.7744 0124271 32.5529 328.3243 14.41383081484436
| Epoch (UTC): | 02 October 2022 21:20:38 |
| Eccentricity: | 0.0124271 |
| inclination: | 99.1251° |
| perigee height: | 665 km |
| apogee height: | 842 km |
| right ascension of ascending node: | 309.7744° |
| argument of perigee: | 32.5529° |
| revolutions per day: | 14.41383081 |
| mean anomaly at epoch: | 328.3243° |
| orbit number at epoch: | 48443 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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