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 56094U 26145.19154418 +.00000000 +00000-0 +29110-4 0 00005
2 56094 43.0033 89.3301 0001103 265.3143 94.7582 15.27577346 04
| Epoch (UTC): | 25 May 2026 04:35:49 |
| Eccentricity: | 0.0001103 |
| inclination: | 43.0033° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 89.3301° |
| argument of perigee: | 265.3143° |
| revolutions per day: | 15.27577346 |
| mean anomaly at epoch: | 94.7582° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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