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 55342U 26145.28676813 +.00000000 +00000-0 -64710-4 0 00004
2 55342 43.0043 231.1960 0001688 267.4393 92.6265 15.27596912 01
| Epoch (UTC): | 25 May 2026 06:52:56 |
| Eccentricity: | 0.0001688 |
| inclination: | 43.0043° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 231.1960° |
| argument of perigee: | 267.4393° |
| revolutions per day: | 15.27596912 |
| mean anomaly at epoch: | 92.6265° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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