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 44768C 19074BH 20221.46905514 -.00001198 00000-0 -82048-4 0 2216
2 44768 52.9997 21.0336 0001201 109.1962 354.4717 15.05588257 17
| Epoch (UTC): | 08 August 2020 11:15:26 |
| Eccentricity: | 0.0001201 |
| inclination: | 52.9997° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 21.0336° |
| argument of perigee: | 109.1962° |
| revolutions per day: | 15.05588257 |
| mean anomaly at epoch: | 354.4717° |
| orbit number at epoch: | 1 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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