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 56011U 26145.56247919 +.00000000 +00000-0 -15443-4 0 00009
2 56011 43.0060 330.9708 0001530 279.0113 81.0566 15.27573227 07
| Epoch (UTC): | 25 May 2026 13:29:58 |
| Eccentricity: | 0.0001530 |
| inclination: | 43.0060° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 330.9708° |
| argument of perigee: | 279.0113° |
| revolutions per day: | 15.27573227 |
| mean anomaly at epoch: | 81.0566° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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