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 56096U 26145.52233036 +.00000000 +00000-0 +21110-4 0 00000
2 56096 43.0039 87.5131 0001178 265.7570 94.3147 15.27577439 09
| Epoch (UTC): | 25 May 2026 12:32:09 |
| Eccentricity: | 0.0001178 |
| inclination: | 43.0039° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 87.5131° |
| argument of perigee: | 265.7570° |
| revolutions per day: | 15.27577439 |
| mean anomaly at epoch: | 94.3147° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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