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 55583U 26145.10587487 +.00000000 +00000-0 +89593-5 0 00006
2 55583 42.9961 293.3000 0001883 290.0659 69.9990 15.27586789 07
| Epoch (UTC): | 25 May 2026 02:32:27 |
| Eccentricity: | 0.0001883 |
| inclination: | 42.9961° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 293.3000° |
| argument of perigee: | 290.0659° |
| revolutions per day: | 15.27586789 |
| mean anomaly at epoch: | 69.9990° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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