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 21017.56265996 -.00000055 00000-0 19207-4 0 9990
2 00022 50.2828 177.3055 0138875 356.9135 3.0943 14.95383424502406
| Epoch (UTC): | 17 January 2021 13:30:13 |
| Eccentricity: | 0.0138875 |
| inclination: | 50.2828° |
| perigee height: | 484 km |
| apogee height: | 678 km |
| right ascension of ascending node: | 177.3055° |
| argument of perigee: | 356.9135° |
| revolutions per day: | 14.95383424 |
| mean anomaly at epoch: | 3.0943° |
| orbit number at epoch: | 50240 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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