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 62685U 26145.15634726 +.00000000 +00000-0 +24316-3 0 00001
2 62685 97.3948 225.2964 0006719 62.8118 297.3805 15.25151826 08
| Epoch (UTC): | 25 May 2026 03:45:08 |
| Eccentricity: | 0.0006719 |
| inclination: | 97.3948° |
| perigee height: | 486 km |
| apogee height: | 495 km |
| right ascension of ascending node: | 225.2964° |
| argument of perigee: | 62.8118° |
| revolutions per day: | 15.25151826 |
| mean anomaly at epoch: | 297.3805° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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