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 25134U 98002A 23334.76005391 .00000061 00000-0 00000+0 0 9996
2 25134 12.1791 16.2297 0005530 149.6427 224.8976 0.99151645 94226
| Epoch (UTC): | 30 November 2023 18:14:28 |
| Eccentricity: | 0.0005530 |
| inclination: | 12.1791° |
| perigee height: | 36079 km |
| apogee height: | 36126 km |
| right ascension of ascending node: | 16.2297° |
| argument of perigee: | 149.6427° |
| revolutions per day: | 0.99151645 |
| mean anomaly at epoch: | 224.8976° |
| orbit number at epoch: | 9422 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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