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 64911U 26144.99448023 +.00000000 +00000-0 +76869-3 0 00009
2 64911 53.1594 351.4348 0000528 28.4370 331.6659 15.30199550 08
| Epoch (UTC): | 24 May 2026 23:52:03 |
| Eccentricity: | 0.0000528 |
| inclination: | 53.1594° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 351.4348° |
| argument of perigee: | 28.4370° |
| revolutions per day: | 15.30199550 |
| mean anomaly at epoch: | 331.6659° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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