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 56711U 26145.24983444 +.00000000 +00000-0 +14368-3 0 00004
2 56711 87.9111 233.3258 0002287 112.8642 247.2730 13.16592643 03
| Epoch (UTC): | 25 May 2026 05:59:45 |
| Eccentricity: | 0.0002287 |
| inclination: | 87.9111° |
| perigee height: | 1196 km |
| apogee height: | 1199 km |
| right ascension of ascending node: | 233.3258° |
| argument of perigee: | 112.8642° |
| revolutions per day: | 13.16592643 |
| mean anomaly at epoch: | 247.2730° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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