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 56108U 26145.52747874 +.00000000 +00000-0 +99239-4 0 00001
2 56108 43.0006 87.5415 0000935 248.8177 111.2574 15.27584521 00
| Epoch (UTC): | 25 May 2026 12:39:34 |
| Eccentricity: | 0.0000935 |
| inclination: | 43.0006° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 87.5415° |
| argument of perigee: | 248.8177° |
| revolutions per day: | 15.27584521 |
| mean anomaly at epoch: | 111.2574° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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