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 62251U 24232Q 24358.12953526 .00001264 00000-0 52415-3 0 9997
2 62251 88.9935 78.0795 0016787 155.4524 204.7472 14.25912664 19513
| Epoch (UTC): | 23 December 2024 03:06:31 |
| Eccentricity: | 0.0016787 |
| inclination: | 88.9935° |
| perigee height: | 793 km |
| apogee height: | 817 km |
| right ascension of ascending node: | 78.0795° |
| argument of perigee: | 155.4524° |
| revolutions per day: | 14.25912664 |
| mean anomaly at epoch: | 204.7472° |
| orbit number at epoch: | 1951 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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