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 55498U 26145.39890330 +.00000000 +00000-0 +32236-4 0 00007
2 55498 43.0023 266.7931 0002106 280.4171 79.6443 15.27577054 07
| Epoch (UTC): | 25 May 2026 09:34:25 |
| Eccentricity: | 0.0002106 |
| inclination: | 43.0023° |
| perigee height: | 482 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 266.7931° |
| argument of perigee: | 280.4171° |
| revolutions per day: | 15.27577054 |
| mean anomaly at epoch: | 79.6443° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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