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 00116U 61015A 21025.37869584 -.00000063 00000-0 10400-4 0 9990
2 00116 66.8106 25.6819 0079507 217.5463 142.0049 13.91781966 22706
| Epoch (UTC): | 25 January 2021 09:05:19 |
| Eccentricity: | 0.0079507 |
| inclination: | 66.8106° |
| perigee height: | 864 km |
| apogee height: | 980 km |
| right ascension of ascending node: | 25.6819° |
| argument of perigee: | 217.5463° |
| revolutions per day: | 13.91781966 |
| mean anomaly at epoch: | 142.0049° |
| orbit number at epoch: | 2270 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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