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 55582U 26040.35207932 +.00000000 +00000-0 -16300-3 0 00005
2 55582 43.0031 145.9017 0001400 274.2910 85.7773 15.02512746 05
| Epoch (UTC): | 09 February 2026 08:26:59 |
| Eccentricity: | 0.0001400 |
| inclination: | 43.0031° |
| perigee height: | 558 km |
| apogee height: | 560 km |
| right ascension of ascending node: | 145.9017° |
| argument of perigee: | 274.2910° |
| revolutions per day: | 15.02512746 |
| mean anomaly at epoch: | 85.7773° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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