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 61922U 26145.54543757 +.00000000 +00000-0 +37702-3 0 00003
2 61922 42.9997 211.3775 0001491 274.1487 85.9194 15.27587365 01
| Epoch (UTC): | 25 May 2026 13:05:25 |
| Eccentricity: | 0.0001491 |
| inclination: | 42.9997° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 211.3775° |
| argument of perigee: | 274.1487° |
| revolutions per day: | 15.27587365 |
| mean anomaly at epoch: | 85.9194° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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