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 20104U 89050B 24278.69384187 .00000303 00000-0 28808-3 0 9993
2 20104 82.9607 352.4841 0042188 275.0705 84.5638 13.77502275771454
| Epoch (UTC): | 04 October 2024 16:39:07 |
| Eccentricity: | 0.0042188 |
| inclination: | 82.9607° |
| perigee height: | 942 km |
| apogee height: | 1004 km |
| right ascension of ascending node: | 352.4841° |
| argument of perigee: | 275.0705° |
| revolutions per day: | 13.77502275 |
| mean anomaly at epoch: | 84.5638° |
| orbit number at epoch: | 77145 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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