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 54855U 26145.12600704 +.00000000 +00000-0 +27107-5 0 00000
2 54855 43.0068 49.6476 0001617 272.8937 87.1729 15.27574296 01
| Epoch (UTC): | 25 May 2026 03:01:27 |
| Eccentricity: | 0.0001617 |
| inclination: | 43.0068° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 49.6476° |
| argument of perigee: | 272.8937° |
| revolutions per day: | 15.27574296 |
| mean anomaly at epoch: | 87.1729° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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