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 23038.59674013 .00006316 00000-0 45263-3 0 9997
2 00022 50.2797 246.1413 0129755 352.4076 7.4906 14.99015436614877
| Epoch (UTC): | 07 February 2023 14:19:18 |
| Eccentricity: | 0.0129755 |
| inclination: | 50.2797° |
| perigee height: | 480 km |
| apogee height: | 660 km |
| right ascension of ascending node: | 246.1413° |
| argument of perigee: | 352.4076° |
| revolutions per day: | 14.99015436 |
| mean anomaly at epoch: | 7.4906° |
| orbit number at epoch: | 61487 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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