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 24276.29684688 .00000292 00000-0 27673-3 0 9992
2 20104 82.9610 354.2631 0042150 282.0079 77.6356 13.77501281771126
| Epoch (UTC): | 02 October 2024 07:07:27 |
| Eccentricity: | 0.0042150 |
| inclination: | 82.9610° |
| perigee height: | 942 km |
| apogee height: | 1004 km |
| right ascension of ascending node: | 354.2631° |
| argument of perigee: | 282.0079° |
| revolutions per day: | 13.77501281 |
| mean anomaly at epoch: | 77.6356° |
| orbit number at epoch: | 77112 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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