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 65804U 26145.35984764 +.00000000 +00000-0 +22308-3 0 00008
2 65804 97.4520 8.1011 0002635 81.8219 278.3307 15.05656841 09
| Epoch (UTC): | 25 May 2026 08:38:10 |
| Eccentricity: | 0.0002635 |
| inclination: | 97.4520° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 8.1011° |
| argument of perigee: | 81.8219° |
| revolutions per day: | 15.05656841 |
| mean anomaly at epoch: | 278.3307° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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