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 23160.91633703 .00007733 00000-0 52760-3 0 9994
2 00022 50.2814 27.9368 0126503 103.5050 258.0030 15.00787883633234
| Epoch (UTC): | 09 June 2023 21:59:31 |
| Eccentricity: | 0.0126503 |
| inclination: | 50.2814° |
| perigee height: | 476 km |
| apogee height: | 652 km |
| right ascension of ascending node: | 27.9368° |
| argument of perigee: | 103.5050° |
| revolutions per day: | 15.00787883 |
| mean anomaly at epoch: | 258.0030° |
| orbit number at epoch: | 63323 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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