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 55466U 26145.34252491 +.00000000 +00000-0 +26850-4 0 00002
2 55466 43.0036 255.9469 0001300 270.6688 89.4015 15.27576453 07
| Epoch (UTC): | 25 May 2026 08:13:14 |
| Eccentricity: | 0.0001300 |
| inclination: | 43.0036° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 255.9469° |
| argument of perigee: | 270.6688° |
| revolutions per day: | 15.27576453 |
| mean anomaly at epoch: | 89.4015° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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