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 22U 59009A 23029.13011004 .00005518 00000-0 39903-3 0 9999
2 22 50.2820 290.8224 0129985 316.0345 43.0320 14.98914884368416
| Epoch (UTC): | 29 January 2023 03:07:21 |
| Eccentricity: | 0.0129985 |
| inclination: | 50.2820° |
| perigee height: | 480 km |
| apogee height: | 660 km |
| right ascension of ascending node: | 290.8224° |
| argument of perigee: | 316.0345° |
| revolutions per day: | 14.98914884 |
| mean anomaly at epoch: | 43.0320° |
| orbit number at epoch: | 36841 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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