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 65974U 26145.52045766 +.00000000 +00000-0 +13912-3 0 00006
2 65974 81.3003 233.1483 0001326 102.9826 257.1476 13.79935896 04
| Epoch (UTC): | 25 May 2026 12:29:27 |
| Eccentricity: | 0.0001326 |
| inclination: | 81.3003° |
| perigee height: | 963 km |
| apogee height: | 965 km |
| right ascension of ascending node: | 233.1483° |
| argument of perigee: | 102.9826° |
| revolutions per day: | 13.79935896 |
| mean anomaly at epoch: | 257.1476° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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