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 116U 61015A 20025.82279655 -.00000075 00000-0 10388-5 0 9992
2 116 66.8080 199.3281 0069482 111.2992 249.5524 13.91764798972324
| Epoch (UTC): | 25 January 2020 19:44:49 |
| Eccentricity: | 0.0069482 |
| inclination: | 66.8080° |
| perigee height: | 872 km |
| apogee height: | 973 km |
| right ascension of ascending node: | 199.3281° |
| argument of perigee: | 111.2992° |
| revolutions per day: | 13.91764798 |
| mean anomaly at epoch: | 249.5524° |
| orbit number at epoch: | 97232 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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