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 19339.44186304 -.00000059 00000-0 13927-4 0 9997
2 116 66.8099 324.9294 0072219 150.0973 210.4262 13.91761697965172
| Epoch (UTC): | 05 December 2019 10:36:16 |
| Eccentricity: | 0.0072219 |
| inclination: | 66.8099° |
| perigee height: | 870 km |
| apogee height: | 975 km |
| right ascension of ascending node: | 324.9294° |
| argument of perigee: | 150.0973° |
| revolutions per day: | 13.91761697 |
| mean anomaly at epoch: | 210.4262° |
| orbit number at epoch: | 96517 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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