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 24129U 26087.90400788 +.00000000 +00000-0 +61229-3 0 00003
2 24129 81.4745 234.9641 0538735 278.6114 201.6682 13.89241599 04
| Epoch (UTC): | 28 March 2026 21:41:46 |
| Eccentricity: | 0.0538735 |
| inclination: | 81.4745° |
| perigee height: | 538 km |
| apogee height: | 1325 km |
| right ascension of ascending node: | 234.9641° |
| argument of perigee: | 278.6114° |
| revolutions per day: | 13.89241599 |
| mean anomaly at epoch: | 201.6682° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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