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 24278.80278450 .00016675 00000-0 12740-2 0 9990
2 20682 63.2969 76.5300 0906508 70.9433 298.7483 13.55033472 19420
| Epoch (UTC): | 04 October 2024 19:16:00 |
| Eccentricity: | 0.0906508 |
| inclination: | 63.2969° |
| perigee height: | 380 km |
| apogee height: | 1727 km |
| right ascension of ascending node: | 76.5300° |
| argument of perigee: | 70.9433° |
| revolutions per day: | 13.55033472 |
| mean anomaly at epoch: | 298.7483° |
| orbit number at epoch: | 1942 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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