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 22590U 26104.18161440 +.00000000 +00000-0 +31499-4 0 00009
2 22590 82.9347 188.2830 0024436 111.3235 275.4366 13.75630447 01
| Epoch (UTC): | 14 April 2026 04:21:31 |
| Eccentricity: | 0.0024436 |
| inclination: | 82.9347° |
| perigee height: | 961 km |
| apogee height: | 997 km |
| right ascension of ascending node: | 188.2830° |
| argument of perigee: | 111.3235° |
| revolutions per day: | 13.75630447 |
| mean anomaly at epoch: | 275.4366° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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