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 24126U 26087.94975439 +.00000000 +00000-0 +21841-2 0 00009
2 24126 81.7984 60.1707 0275125 54.3926 359.5064 14.41433400 02
| Epoch (UTC): | 28 March 2026 22:47:38 |
| Eccentricity: | 0.0275125 |
| inclination: | 81.7984° |
| perigee height: | 558 km |
| apogee height: | 950 km |
| right ascension of ascending node: | 60.1707° |
| argument of perigee: | 54.3926° |
| revolutions per day: | 14.41433400 |
| mean anomaly at epoch: | 359.5064° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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