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 55481U 26145.38734054 +.00000000 +00000-0 -75133-6 0 00004
2 55481 43.0036 266.7219 0001251 289.5508 70.5208 15.27577583 02
| Epoch (UTC): | 25 May 2026 09:17:46 |
| Eccentricity: | 0.0001251 |
| inclination: | 43.0036° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 266.7219° |
| argument of perigee: | 289.5508° |
| revolutions per day: | 15.27577583 |
| mean anomaly at epoch: | 70.5208° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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