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 59922U 26145.35367185 +.00000000 +00000-0 +16972-4 0 00005
2 59922 43.0004 259.9030 0001137 276.0871 83.9851 15.27575640 07
| Epoch (UTC): | 25 May 2026 08:29:17 |
| Eccentricity: | 0.0001137 |
| inclination: | 43.0004° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 259.9030° |
| argument of perigee: | 276.0871° |
| revolutions per day: | 15.27575640 |
| mean anomaly at epoch: | 83.9851° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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