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 55366U 26145.50257733 +.00000000 +00000-0 -45806-6 0 00008
2 55366 42.9998 214.6694 0001125 276.6818 83.3905 15.27577128 00
| Epoch (UTC): | 25 May 2026 12:03:42 |
| Eccentricity: | 0.0001125 |
| inclination: | 42.9998° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 214.6694° |
| argument of perigee: | 276.6818° |
| revolutions per day: | 15.27577128 |
| mean anomaly at epoch: | 83.3905° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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