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 64332U 26145.00809014 +.00000000 +00000-0 +75530-3 0 00004
2 64332 43.0002 50.5808 0001492 245.2501 114.8196 15.27566246 04
| Epoch (UTC): | 25 May 2026 00:11:38 |
| Eccentricity: | 0.0001492 |
| inclination: | 43.0002° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 50.5808° |
| argument of perigee: | 245.2501° |
| revolutions per day: | 15.27566246 |
| mean anomaly at epoch: | 114.8196° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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