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 19168.84209079 -.00000066 00000-0 83171-5 0 9993
2 116 66.8106 21.9789 0082745 265.5842 93.5780 13.91753878941425
| Epoch (UTC): | 17 June 2019 20:12:36 |
| Eccentricity: | 0.0082745 |
| inclination: | 66.8106° |
| perigee height: | 862 km |
| apogee height: | 983 km |
| right ascension of ascending node: | 21.9789° |
| argument of perigee: | 265.5842° |
| revolutions per day: | 13.91753878 |
| mean anomaly at epoch: | 93.5780° |
| orbit number at epoch: | 94142 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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