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 55353U 26145.56796199 +.00000000 +00000-0 +12531-3 0 00009
2 55353 43.0017 225.5979 0001331 288.3894 71.6813 15.27584576 03
| Epoch (UTC): | 25 May 2026 13:37:51 |
| Eccentricity: | 0.0001331 |
| inclination: | 43.0017° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 225.5979° |
| argument of perigee: | 288.3894° |
| revolutions per day: | 15.27584576 |
| mean anomaly at epoch: | 71.6813° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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