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 57543U 74025J 24357.28530903 .00012326 00000-0 63020-2 0 9990
2 57543 81.2049 103.4809 0006612 97.7885 262.4040 14.15458651 80707
| Epoch (UTC): | 22 December 2024 06:50:50 |
| Eccentricity: | 0.0006612 |
| inclination: | 81.2049° |
| perigee height: | 836 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 103.4809° |
| argument of perigee: | 97.7885° |
| revolutions per day: | 14.15458651 |
| mean anomaly at epoch: | 262.4040° |
| orbit number at epoch: | 8070 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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