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 20150U 89059B 24357.72617868 .00000036 00000-0 21152-4 0 9999
2 20150 82.9402 217.2398 0028816 172.7893 253.0673 13.75852252777668
| Epoch (UTC): | 22 December 2024 17:25:41 |
| Eccentricity: | 0.0028816 |
| inclination: | 82.9402° |
| perigee height: | 957 km |
| apogee height: | 1000 km |
| right ascension of ascending node: | 217.2398° |
| argument of perigee: | 172.7893° |
| revolutions per day: | 13.75852252 |
| mean anomaly at epoch: | 253.0673° |
| orbit number at epoch: | 77766 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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