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 56891U 26145.66668980 +.00000000 +00000-0 +36374-3 0 00005
2 56891 43.0013 10.2239 0001264 253.9679 185.0718 15.27579013 03
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001264 |
| inclination: | 43.0013° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 10.2239° |
| argument of perigee: | 253.9679° |
| revolutions per day: | 15.27579013 |
| mean anomaly at epoch: | 185.0718° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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