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 23787U 96009A 23083.94406529 .00000044 00000-0 18252-3 0 9995
2 23787 82.5801 334.6313 0010375 200.4899 170.4242 12.64060310250194
| Epoch (UTC): | 24 March 2023 22:39:27 |
| Eccentricity: | 0.0010375 |
| inclination: | 82.5801° |
| perigee height: | 1398 km |
| apogee height: | 1414 km |
| right ascension of ascending node: | 334.6313° |
| argument of perigee: | 200.4899° |
| revolutions per day: | 12.64060310 |
| mean anomaly at epoch: | 170.4242° |
| orbit number at epoch: | 25019 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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