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 00022U 59009A 21067.81440692 .00000276 00000-0 43370-4 0 9993
2 00022 50.2840 301.4223 0138792 188.9421 170.9050 14.95429588509925
| Epoch (UTC): | 08 March 2021 19:32:44 |
| Eccentricity: | 0.0138792 |
| inclination: | 50.2840° |
| perigee height: | 484 km |
| apogee height: | 677 km |
| right ascension of ascending node: | 301.4223° |
| argument of perigee: | 188.9421° |
| revolutions per day: | 14.95429588 |
| mean anomaly at epoch: | 170.9050° |
| orbit number at epoch: | 50992 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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