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 53622U 26145.54805961 +.00000000 +00000-0 +39839-4 0 00003
2 53622 53.2134 248.6957 0001219 80.6620 279.4510 15.08840199 07
| Epoch (UTC): | 25 May 2026 13:09:12 |
| Eccentricity: | 0.0001219 |
| inclination: | 53.2134° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 248.6957° |
| argument of perigee: | 80.6620° |
| revolutions per day: | 15.08840199 |
| mean anomaly at epoch: | 279.4510° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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