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 62865U 26145.26248703 +.00000000 +00000-0 +54643-3 0 00005
2 62865 53.1566 133.9523 0001062 94.6542 265.4580 15.30184656 09
| Epoch (UTC): | 25 May 2026 06:17:58 |
| Eccentricity: | 0.0001062 |
| inclination: | 53.1566° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 133.9523° |
| argument of perigee: | 94.6542° |
| revolutions per day: | 15.30184656 |
| mean anomaly at epoch: | 265.4580° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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