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 55500U 26145.32709058 +.00000000 +00000-0 +18002-4 0 00005
2 55500 43.0053 267.1146 0002086 281.5444 78.5174 15.27575406 07
| Epoch (UTC): | 25 May 2026 07:51:00 |
| Eccentricity: | 0.0002086 |
| inclination: | 43.0053° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 267.1146° |
| argument of perigee: | 281.5444° |
| revolutions per day: | 15.27575406 |
| mean anomaly at epoch: | 78.5174° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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