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 44762C 19074BB 21016.82461973 .00001299 00000-0 87033-4 0 160
2 44762 53.0597 356.6719 0002022 62.4403 181.3853 15.06392300 15
| Epoch (UTC): | 16 January 2021 19:47:27 |
| Eccentricity: | 0.0002022 |
| inclination: | 53.0597° |
| perigee height: | 546 km |
| apogee height: | 548 km |
| right ascension of ascending node: | 356.6719° |
| argument of perigee: | 62.4403° |
| revolutions per day: | 15.06392300 |
| mean anomaly at epoch: | 181.3853° |
| 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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