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 55468U 26145.33481241 +.00000000 +00000-0 +69369-4 0 00002
2 55468 43.0005 255.8872 0001358 266.7123 93.3573 15.27574196 00
| Epoch (UTC): | 25 May 2026 08:02:07 |
| Eccentricity: | 0.0001358 |
| inclination: | 43.0005° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 255.8872° |
| argument of perigee: | 266.7123° |
| revolutions per day: | 15.27574196 |
| mean anomaly at epoch: | 93.3573° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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