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 55386U 26145.54525595 +.00000000 +00000-0 +10937-4 0 00002
2 55386 43.0046 244.3735 0001991 279.8832 80.1795 15.27580005 06
| Epoch (UTC): | 25 May 2026 13:05:10 |
| Eccentricity: | 0.0001991 |
| inclination: | 43.0046° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 244.3735° |
| argument of perigee: | 279.8832° |
| revolutions per day: | 15.27580005 |
| mean anomaly at epoch: | 80.1795° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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