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 55381U 26145.60678978 +.00000000 +00000-0 +47155-4 0 00000
2 55381 43.0025 243.9777 0001525 282.3481 77.7200 15.27582359 08
| Epoch (UTC): | 25 May 2026 14:33:46 |
| Eccentricity: | 0.0001525 |
| inclination: | 43.0025° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 243.9777° |
| argument of perigee: | 282.3481° |
| revolutions per day: | 15.27582359 |
| mean anomaly at epoch: | 77.7200° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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