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 42508U 70025RN 24353.28759808 .00000933 00000-0 72495-3 0 9992
2 42508 99.8600 180.9821 0122012 348.0324 11.7941 13.91977716100537
| Epoch (UTC): | 18 December 2024 06:54:08 |
| Eccentricity: | 0.0122012 |
| inclination: | 99.8600° |
| perigee height: | 832 km |
| apogee height: | 1011 km |
| right ascension of ascending node: | 180.9821° |
| argument of perigee: | 348.0324° |
| revolutions per day: | 13.91977716 |
| mean anomaly at epoch: | 11.7941° |
| orbit number at epoch: | 10053 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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