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 21016.37541244 -.00000098 00000-0 -29719-4 0 9992
2 00082 38.8549 129.9655 1174832 31.2046 335.3300 12.26049427833949
| Epoch (UTC): | 16 January 2021 09:00:35 |
| Eccentricity: | 0.1174832 |
| inclination: | 38.8549° |
| perigee height: | 633 km |
| apogee height: | 2499 km |
| right ascension of ascending node: | 129.9655° |
| argument of perigee: | 31.2046° |
| revolutions per day: | 12.26049427 |
| mean anomaly at epoch: | 335.3300° |
| orbit number at epoch: | 83394 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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