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 36605U 10030A 22267.51869912 .00001509 00000-0 75041-4 0 9990
2 36605 97.4462 273.7148 0001698 85.7827 33.1167 15.19151796679904
| Epoch (UTC): | 24 September 2022 12:26:55 |
| Eccentricity: | 0.0001698 |
| inclination: | 97.4462° |
| perigee height: | 507 km |
| apogee height: | 509 km |
| right ascension of ascending node: | 273.7148° |
| argument of perigee: | 85.7827° |
| revolutions per day: | 15.19151796 |
| mean anomaly at epoch: | 33.1167° |
| orbit number at epoch: | 67990 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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