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 19348.85572633 -.00000036 +00000-0 +31417-4 0 9995
2 116 066.8103 301.9164 0071536 143.1115 217.4916 13.91762322965990
| Epoch (UTC): | 14 December 2019 20:32:14 |
| Eccentricity: | 0.0071536 |
| inclination: | 66.8103° |
| perigee height: | 870 km |
| apogee height: | 974 km |
| right ascension of ascending node: | 301.9164° |
| argument of perigee: | 143.1115° |
| revolutions per day: | 13.91762322 |
| mean anomaly at epoch: | 217.4916° |
| orbit number at epoch: | 96599 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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