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 19342.67563345 -.00000056 +00000-0 +15781-4 0 9997
2 116 066.8100 317.0241 0071969 147.6969 212.8548 13.91761840965137
| Epoch (UTC): | 08 December 2019 16:12:54 |
| Eccentricity: | 0.0071969 |
| inclination: | 66.8100° |
| perigee height: | 870 km |
| apogee height: | 975 km |
| right ascension of ascending node: | 317.0241° |
| argument of perigee: | 147.6969° |
| revolutions per day: | 13.91761840 |
| mean anomaly at epoch: | 212.8548° |
| orbit number at epoch: | 96513 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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