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 21022.77511083 -.00000002 00000-0 23163-4 0 9998
2 00022 50.2834 152.8390 0138853 16.8293 343.7194 14.95386694503186
| Epoch (UTC): | 22 January 2021 18:36:09 |
| Eccentricity: | 0.0138853 |
| inclination: | 50.2834° |
| perigee height: | 484 km |
| apogee height: | 678 km |
| right ascension of ascending node: | 152.8390° |
| argument of perigee: | 16.8293° |
| revolutions per day: | 14.95386694 |
| mean anomaly at epoch: | 343.7194° |
| orbit number at epoch: | 50318 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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