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 20022.51717526 -.00000051 00000-0 19477-4 0 9990
2 116 66.8078 207.4088 0069583 113.8337 247.0056 13.91764660971869
| Epoch (UTC): | 22 January 2020 12:24:43 |
| Eccentricity: | 0.0069583 |
| inclination: | 66.8078° |
| perigee height: | 871 km |
| apogee height: | 973 km |
| right ascension of ascending node: | 207.4088° |
| argument of perigee: | 113.8337° |
| revolutions per day: | 13.91764660 |
| mean anomaly at epoch: | 247.0056° |
| orbit number at epoch: | 97186 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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