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 56834U 26145.55527889 +.00000000 +00000-0 +55493-4 0 00006
2 56834 43.0041 29.5615 0001476 274.5226 85.5457 15.27591924 03
| Epoch (UTC): | 25 May 2026 13:19:36 |
| Eccentricity: | 0.0001476 |
| inclination: | 43.0041° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 29.5615° |
| argument of perigee: | 274.5226° |
| revolutions per day: | 15.27591924 |
| mean anomaly at epoch: | 85.5457° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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