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 55605U 26145.41112828 +.00000000 +00000-0 +78613-5 0 00009
2 55605 43.0014 280.8820 0000945 273.6083 86.4660 15.27573744 05
| Epoch (UTC): | 25 May 2026 09:52:01 |
| Eccentricity: | 0.0000945 |
| inclination: | 43.0014° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 280.8820° |
| argument of perigee: | 273.6083° |
| revolutions per day: | 15.27573744 |
| mean anomaly at epoch: | 86.4660° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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