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 20103U 89050A 23333.35965916 .00000107 00000-0 96010-4 0 9994
2 20103 82.9602 268.9824 0037211 182.5250 298.1729 13.74696389725559
| Epoch (UTC): | 29 November 2023 08:37:54 |
| Eccentricity: | 0.0037211 |
| inclination: | 82.9602° |
| perigee height: | 955 km |
| apogee height: | 1010 km |
| right ascension of ascending node: | 268.9824° |
| argument of perigee: | 182.5250° |
| revolutions per day: | 13.74696389 |
| mean anomaly at epoch: | 298.1729° |
| orbit number at epoch: | 72555 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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