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 is defined by the following mean orbital elements,
1 24602U 26088.18719028 +.00000000 +00000-0 +21184-2 0 00005
2 24602 81.5210 260.6675 0728929 213.2923 142.0306 13.44765064 00
| Epoch (UTC): | 29 March 2026 04:29:33 |
| Eccentricity: | 0.0728929 |
| inclination: | 81.5210° |
| perigee height: | 547 km |
| apogee height: | 1636 km |
| right ascension of ascending node: | 260.6675° |
| argument of perigee: | 213.2923° |
| revolutions per day: | 13.44765064 |
| mean anomaly at epoch: | 142.0306° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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