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 21024.60558173 -.00000127 00000-0 -50846-4 0 9994
2 00082 38.8562 99.4889 1174829 70.9468 301.4599 12.26048722834951
| Epoch (UTC): | 24 January 2021 14:32:02 |
| Eccentricity: | 0.1174829 |
| inclination: | 38.8562° |
| perigee height: | 633 km |
| apogee height: | 2499 km |
| right ascension of ascending node: | 99.4889° |
| argument of perigee: | 70.9468° |
| revolutions per day: | 12.26048722 |
| mean anomaly at epoch: | 301.4599° |
| orbit number at epoch: | 83495 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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