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 56907U 26145.59517456 +.00000000 +00000-0 +34656-4 0 00008
2 56907 43.0040 356.0379 0001432 264.7942 95.2746 15.27577454 07
| Epoch (UTC): | 25 May 2026 14:17:03 |
| Eccentricity: | 0.0001432 |
| inclination: | 43.0040° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 356.0379° |
| argument of perigee: | 264.7942° |
| revolutions per day: | 15.27577454 |
| mean anomaly at epoch: | 95.2746° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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