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 26106.97521090 +.00000000 +00000-0 +43538-4 0 00006
2 22590 82.9345 186.2095 0024492 103.9660 69.6361 13.75630574 00
| Epoch (UTC): | 16 April 2026 23:24:18 |
| Eccentricity: | 0.0024492 |
| inclination: | 82.9345° |
| perigee height: | 961 km |
| apogee height: | 997 km |
| right ascension of ascending node: | 186.2095° |
| argument of perigee: | 103.9660° |
| revolutions per day: | 13.75630574 |
| mean anomaly at epoch: | 69.6361° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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