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 64841U 26145.56981352 +.00000000 +00000-0 +54617-3 0 00009
2 64841 97.7669 261.8248 0008297 291.3578 68.6760 14.99730024 03
| Epoch (UTC): | 25 May 2026 13:40:31 |
| Eccentricity: | 0.0008297 |
| inclination: | 97.7669° |
| perigee height: | 562 km |
| apogee height: | 573 km |
| right ascension of ascending node: | 261.8248° |
| argument of perigee: | 291.3578° |
| revolutions per day: | 14.99730024 |
| mean anomaly at epoch: | 68.6760° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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