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 52159U 22033C 23150.85648492 .00000512 00000-0 83729-4 0 9990
2 52159 97.9807 233.0840 0005004 16.0410 344.0957 14.74930988 62547
| Epoch (UTC): | 30 May 2023 20:33:20 |
| Eccentricity: | 0.0005004 |
| inclination: | 97.9807° |
| perigee height: | 642 km |
| apogee height: | 649 km |
| right ascension of ascending node: | 233.0840° |
| argument of perigee: | 16.0410° |
| revolutions per day: | 14.74930988 |
| mean anomaly at epoch: | 344.0957° |
| orbit number at epoch: | 6254 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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