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 20023.52323399 -.00000055 00000-0 16404-4 0 9994
2 116 66.8079 204.9494 0069547 113.0615 247.7817 13.91764720972000
| Epoch (UTC): | 23 January 2020 12:33:27 |
| Eccentricity: | 0.0069547 |
| inclination: | 66.8079° |
| perigee height: | 871 km |
| apogee height: | 973 km |
| right ascension of ascending node: | 204.9494° |
| argument of perigee: | 113.0615° |
| revolutions per day: | 13.91764720 |
| mean anomaly at epoch: | 247.7817° |
| orbit number at epoch: | 97200 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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