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 43937U 19003F 23083.83373049 .00054569 00000-0 11918-2 0 9993
2 43937 97.0986 112.5657 0014513 215.2889 144.7400 15.43905656232992
| Epoch (UTC): | 24 March 2023 20:00:34 |
| Eccentricity: | 0.0014513 |
| inclination: | 97.0986° |
| perigee height: | 425 km |
| apogee height: | 444 km |
| right ascension of ascending node: | 112.5657° |
| argument of perigee: | 215.2889° |
| revolutions per day: | 15.43905656 |
| mean anomaly at epoch: | 144.7400° |
| orbit number at epoch: | 23299 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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