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 68576U 26145.58335647 +.00000000 +00000-0 +79756-5 0 00003
2 68576 51.8805 286.4250 0003383 279.9463 336.3818 15.27017302 05
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0003383 |
| inclination: | 51.8805° |
| perigee height: | 482 km |
| apogee height: | 487 km |
| right ascension of ascending node: | 286.4250° |
| argument of perigee: | 279.9463° |
| revolutions per day: | 15.27017302 |
| mean anomaly at epoch: | 336.3818° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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