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 00050U 60009B 21112.82220779 -.00000082 00000-0 30191-4 0 9993
2 00050 47.2309 241.0924 0114130 167.7676 192.5922 12.20116682707995
| Epoch (UTC): | 22 April 2021 19:43:58 |
| Eccentricity: | 0.0114130 |
| inclination: | 47.2309° |
| perigee height: | 1501 km |
| apogee height: | 1683 km |
| right ascension of ascending node: | 241.0924° |
| argument of perigee: | 167.7676° |
| revolutions per day: | 12.20116682 |
| mean anomaly at epoch: | 192.5922° |
| orbit number at epoch: | 70799 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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