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 20221.85951275 -.00000080 +00000-0 -21292-5 0 9991
2 116 066.8097 080.1073 0079048 327.6494 031.9751 13.91773367999110
| Epoch (UTC): | 08 August 2020 20:37:41 |
| Eccentricity: | 0.0079048 |
| inclination: | 66.8097° |
| perigee height: | 865 km |
| apogee height: | 980 km |
| right ascension of ascending node: | 80.1073° |
| argument of perigee: | 327.6494° |
| revolutions per day: | 13.91773367 |
| mean anomaly at epoch: | 31.9751° |
| orbit number at epoch: | 99911 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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