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 53922U 26145.49656108 +.00000000 +00000-0 +63535-4 0 00007
2 53922 53.2127 329.0700 0001500 92.2614 267.8550 15.08838852 05
| Epoch (UTC): | 25 May 2026 11:55:02 |
| Eccentricity: | 0.0001500 |
| inclination: | 53.2127° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 329.0700° |
| argument of perigee: | 92.2614° |
| revolutions per day: | 15.08838852 |
| mean anomaly at epoch: | 267.8550° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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