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 56105U 26145.54930861 +.00000000 +00000-0 +56746-3 0 00005
2 56105 42.9973 87.7109 0001503 262.3956 97.6725 15.27588534 01
| Epoch (UTC): | 25 May 2026 13:11:00 |
| Eccentricity: | 0.0001503 |
| inclination: | 42.9973° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 87.7109° |
| argument of perigee: | 262.3956° |
| revolutions per day: | 15.27588534 |
| mean anomaly at epoch: | 97.6725° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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