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 55986U 26144.97864235 +.00000000 +00000-0 +64107-4 0 00009
2 55986 43.0021 349.0331 0001525 257.6832 102.3849 15.27577141 01
| Epoch (UTC): | 24 May 2026 23:29:14 |
| Eccentricity: | 0.0001525 |
| inclination: | 43.0021° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 349.0331° |
| argument of perigee: | 257.6832° |
| revolutions per day: | 15.27577141 |
| mean anomaly at epoch: | 102.3849° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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