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 27665U 03005C 21016.45336909 .00000034 00000-0 46963-4 0 9992
2 27665 39.5759 283.1950 0008605 149.1256 19.3820 14.28542227938102
| Epoch (UTC): | 16 January 2021 10:52:51 |
| Eccentricity: | 0.0008605 |
| inclination: | 39.5759° |
| perigee height: | 790 km |
| apogee height: | 803 km |
| right ascension of ascending node: | 283.1950° |
| argument of perigee: | 149.1256° |
| revolutions per day: | 14.28542227 |
| mean anomaly at epoch: | 19.3820° |
| orbit number at epoch: | 93810 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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