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 52322U 26145.60784762 +.00000000 +00000-0 +25558-3 0 00003
2 52322 97.3407 219.1313 0003137 73.0227 287.1350 15.16234765 07
| Epoch (UTC): | 25 May 2026 14:35:18 |
| Eccentricity: | 0.0003137 |
| inclination: | 97.3407° |
| perigee height: | 515 km |
| apogee height: | 519 km |
| right ascension of ascending node: | 219.1313° |
| argument of perigee: | 73.0227° |
| revolutions per day: | 15.16234765 |
| mean anomaly at epoch: | 287.1350° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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