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 62866U 26145.28229097 +.00000000 +00000-0 +66326-3 0 00004
2 62866 53.1596 132.6571 0001445 76.1440 283.9723 15.34418298 09
| Epoch (UTC): | 25 May 2026 06:46:29 |
| Eccentricity: | 0.0001445 |
| inclination: | 53.1596° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 132.6571° |
| argument of perigee: | 76.1440° |
| revolutions per day: | 15.34418298 |
| mean anomaly at epoch: | 283.9723° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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