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 56826U 26145.04067006 +.00000000 +00000-0 +57244-4 0 00007
2 56826 43.0019 35.8047 0001147 262.2749 97.7972 15.27576562 05
| Epoch (UTC): | 25 May 2026 00:58:33 |
| Eccentricity: | 0.0001147 |
| inclination: | 43.0019° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 35.8047° |
| argument of perigee: | 262.2749° |
| revolutions per day: | 15.27576562 |
| mean anomaly at epoch: | 97.7972° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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