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 57537U 74025C 24355.59353216 .00007430 00000-0 37123-2 0 9990
2 57537 81.2049 104.3398 0008600 152.5479 207.6151 14.16674397 73503
| Epoch (UTC): | 20 December 2024 14:14:41 |
| Eccentricity: | 0.0008600 |
| inclination: | 81.2049° |
| perigee height: | 830 km |
| apogee height: | 843 km |
| right ascension of ascending node: | 104.3398° |
| argument of perigee: | 152.5479° |
| revolutions per day: | 14.16674397 |
| mean anomaly at epoch: | 207.6151° |
| orbit number at epoch: | 7350 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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