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 56167U 26145.37971852 +.00000000 +00000-0 +10479-3 0 00002
2 56167 81.0037 93.5750 0007584 25.4144 334.7383 13.85155235 08
| Epoch (UTC): | 25 May 2026 09:06:47 |
| Eccentricity: | 0.0007584 |
| inclination: | 81.0037° |
| perigee height: | 940 km |
| apogee height: | 951 km |
| right ascension of ascending node: | 93.5750° |
| argument of perigee: | 25.4144° |
| revolutions per day: | 13.85155235 |
| mean anomaly at epoch: | 334.7383° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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