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 00082U 61004B 24357.88828508 .00000635 00000-0 56530-3 0 9995
2 00082 38.8510 209.7122 1165599 126.4508 244.9379 12.27319015 10271
| Epoch (UTC): | 22 December 2024 21:19:07 |
| Eccentricity: | 0.1165599 |
| inclination: | 38.8510° |
| perigee height: | 635 km |
| apogee height: | 2486 km |
| right ascension of ascending node: | 209.7122° |
| argument of perigee: | 126.4508° |
| revolutions per day: | 12.27319015 |
| mean anomaly at epoch: | 244.9379° |
| orbit number at epoch: | 1027 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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