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 56294U 26145.03959051 +.00000000 +00000-0 -17664-3 0 00007
2 56294 43.0026 137.9258 0001690 289.2272 70.8397 15.27591781 06
| Epoch (UTC): | 25 May 2026 00:57:00 |
| Eccentricity: | 0.0001690 |
| inclination: | 43.0026° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 137.9258° |
| argument of perigee: | 289.2272° |
| revolutions per day: | 15.27591781 |
| mean anomaly at epoch: | 70.8397° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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