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 30726U 99025ASL 24357.95070126 .00003546 00000-0 20806-2 0 9990
2 30726 99.2520 344.2766 0079885 131.7911 285.2653 14.07221039910593
| Epoch (UTC): | 22 December 2024 22:49:00 |
| Eccentricity: | 0.0079885 |
| inclination: | 99.2520° |
| perigee height: | 811 km |
| apogee height: | 927 km |
| right ascension of ascending node: | 344.2766° |
| argument of perigee: | 131.7911° |
| revolutions per day: | 14.07221039 |
| mean anomaly at epoch: | 285.2653° |
| orbit number at epoch: | 91059 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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