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 00022U 59009A 23336.88904427 .00011012 00000-0 69916-3 0 9995
2 00022 50.2793 273.4382 0121128 63.2045 298.1235 15.03410747659682
| Epoch (UTC): | 02 December 2023 21:20:13 |
| Eccentricity: | 0.0121128 |
| inclination: | 50.2793° |
| perigee height: | 472 km |
| apogee height: | 640 km |
| right ascension of ascending node: | 273.4382° |
| argument of perigee: | 63.2045° |
| revolutions per day: | 15.03410747 |
| mean anomaly at epoch: | 298.1235° |
| orbit number at epoch: | 65968 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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