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 20682U 90050B 24281.68083708 .00015257 00000-0 11656-2 0 9990
2 20682 63.2984 68.8614 0906246 71.0052 298.6880 13.55119463 19815
| Epoch (UTC): | 07 October 2024 16:20:24 |
| Eccentricity: | 0.0906246 |
| inclination: | 63.2984° |
| perigee height: | 380 km |
| apogee height: | 1727 km |
| right ascension of ascending node: | 68.8614° |
| argument of perigee: | 71.0052° |
| revolutions per day: | 13.55119463 |
| mean anomaly at epoch: | 298.6880° |
| orbit number at epoch: | 1981 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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