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 56882U 26145.66264267 +.00000000 +00000-0 +48411-5 0 00002
2 56882 43.0021 10.3913 0000804 262.1417 97.9344 15.27572845 05
| Epoch (UTC): | 25 May 2026 15:54:12 |
| Eccentricity: | 0.0000804 |
| inclination: | 43.0021° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 10.3913° |
| argument of perigee: | 262.1417° |
| revolutions per day: | 15.27572845 |
| mean anomaly at epoch: | 97.9344° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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