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 64916U 26145.58335647 +.00000000 +00000-0 +54940-3 0 00003
2 64916 53.1600 341.3006 0000945 83.4168 76.9393 15.34386900 04
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0000945 |
| inclination: | 53.1600° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 341.3006° |
| argument of perigee: | 83.4168° |
| revolutions per day: | 15.34386900 |
| mean anomaly at epoch: | 76.9393° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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