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 62526U 26145.43614566 +.00000000 +00000-0 +28709-3 0 00006
2 62526 43.0013 143.1886 0001142 267.7001 92.3719 15.27585764 07
| Epoch (UTC): | 25 May 2026 10:28:02 |
| Eccentricity: | 0.0001142 |
| inclination: | 43.0013° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 143.1886° |
| argument of perigee: | 267.7001° |
| revolutions per day: | 15.27585764 |
| mean anomaly at epoch: | 92.3719° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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