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 56708U 26145.42630890 +.00000000 +00000-0 +12814-3 0 00008
2 56708 43.0015 201.2911 0002083 271.7745 88.2869 15.27579207 09
| Epoch (UTC): | 25 May 2026 10:13:53 |
| Eccentricity: | 0.0002083 |
| inclination: | 43.0015° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 201.2911° |
| argument of perigee: | 271.7745° |
| revolutions per day: | 15.27579207 |
| mean anomaly at epoch: | 88.2869° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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