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 64111U 26145.40646830 +.00000000 +00000-0 +61665-3 0 00002
2 64111 53.1604 30.0355 0001251 84.7962 275.3182 15.31715318 08
| Epoch (UTC): | 25 May 2026 09:45:18 |
| Eccentricity: | 0.0001251 |
| inclination: | 53.1604° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 30.0355° |
| argument of perigee: | 84.7962° |
| revolutions per day: | 15.31715318 |
| mean anomaly at epoch: | 275.3182° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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