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 56794U 26145.39438778 +.00000000 +00000-0 +13749-3 0 00008
2 56794 69.9986 131.0369 0003906 266.8679 93.2034 14.98332249 01
| Epoch (UTC): | 25 May 2026 09:27:55 |
| Eccentricity: | 0.0003906 |
| inclination: | 69.9986° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 131.0369° |
| argument of perigee: | 266.8679° |
| revolutions per day: | 14.98332249 |
| mean anomaly at epoch: | 93.2034° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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