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 42511U 70025RR 24357.06556442 .00001441 00000-0 47194-2 0 9997
2 42511 100.1714 300.4651 0458662 83.0823 282.2202 12.72100984514027
| Epoch (UTC): | 22 December 2024 01:34:24 |
| Eccentricity: | 0.0458662 |
| inclination: | 100.1714° |
| perigee height: | 1018 km |
| apogee height: | 1729 km |
| right ascension of ascending node: | 300.4651° |
| argument of perigee: | 83.0823° |
| revolutions per day: | 12.72100984 |
| mean anomaly at epoch: | 282.2202° |
| orbit number at epoch: | 51402 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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