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 19051.92274840 -.00000029 +00000-0 +36939-4 0 9999
2 116 066.8106 307.8012 0077855 342.3380 017.4994 13.91747892924676
| Epoch (UTC): | 20 February 2019 22:08:45 |
| Eccentricity: | 0.0077855 |
| inclination: | 66.8106° |
| perigee height: | 865 km |
| apogee height: | 979 km |
| right ascension of ascending node: | 307.8012° |
| argument of perigee: | 342.3380° |
| revolutions per day: | 13.91747892 |
| mean anomaly at epoch: | 17.4994° |
| orbit number at epoch: | 92467 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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