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 56009U 26145.61273767 +.00000000 +00000-0 +39543-5 0 00009
2 56009 43.0059 348.6118 0001713 269.1025 90.9631 15.27575231 07
| Epoch (UTC): | 25 May 2026 14:42:20 |
| Eccentricity: | 0.0001713 |
| inclination: | 43.0059° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 348.6118° |
| argument of perigee: | 269.1025° |
| revolutions per day: | 15.27575231 |
| mean anomaly at epoch: | 90.9631° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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