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 64246U 26145.54010657 +.00000000 +00000-0 +28479-3 0 00004
2 64246 43.0014 232.9541 0001030 272.1725 87.9009 15.27588348 06
| Epoch (UTC): | 25 May 2026 12:57:45 |
| Eccentricity: | 0.0001030 |
| inclination: | 43.0014° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 232.9541° |
| argument of perigee: | 272.1725° |
| revolutions per day: | 15.27588348 |
| mean anomaly at epoch: | 87.9009° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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