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 55450U 26145.35280639 +.00000000 +00000-0 +18948-4 0 00000
2 55450 43.0013 256.0380 0001431 273.4451 86.6238 15.27575197 03
| Epoch (UTC): | 25 May 2026 08:28:02 |
| Eccentricity: | 0.0001431 |
| inclination: | 43.0013° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 256.0380° |
| argument of perigee: | 273.4451° |
| revolutions per day: | 15.27575197 |
| mean anomaly at epoch: | 86.6238° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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