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 21016.82756972 -.00000054 00000-0 19217-4 0 9997
2 00022 50.2827 180.7560 0138884 354.1066 5.8242 14.95383018502295
| Epoch (UTC): | 16 January 2021 19:51:42 |
| Eccentricity: | 0.0138884 |
| inclination: | 50.2827° |
| perigee height: | 484 km |
| apogee height: | 678 km |
| right ascension of ascending node: | 180.7560° |
| argument of perigee: | 354.1066° |
| revolutions per day: | 14.95383018 |
| mean anomaly at epoch: | 5.8242° |
| orbit number at epoch: | 50229 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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