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 22176.82253434 .00000844 00000-0 25483-3 0 9994
2 31807 99.1299 203.9713 0123450 324.4397 34.8607 14.41173161792210
| Epoch (UTC): | 25 June 2022 19:44:26 |
| Eccentricity: | 0.0123450 |
| inclination: | 99.1299° |
| perigee height: | 666 km |
| apogee height: | 842 km |
| right ascension of ascending node: | 203.9713° |
| argument of perigee: | 324.4397° |
| revolutions per day: | 14.41173161 |
| mean anomaly at epoch: | 34.8607° |
| orbit number at epoch: | 79221 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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