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 56024U 26145.55477389 +.00000000 +00000-0 +44406-5 0 00009
2 56024 43.0038 330.9041 0001055 270.9420 89.1311 15.27574137 07
| Epoch (UTC): | 25 May 2026 13:18:52 |
| Eccentricity: | 0.0001055 |
| inclination: | 43.0038° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 330.9041° |
| argument of perigee: | 270.9420° |
| revolutions per day: | 15.27574137 |
| mean anomaly at epoch: | 89.1311° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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