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 65568U 26145.61542417 +.00000000 +00000-0 +69746-4 0 00007
2 65568 81.3035 31.6408 0007205 250.0375 110.0006 13.83431491 05
| Epoch (UTC): | 25 May 2026 14:46:12 |
| Eccentricity: | 0.0007205 |
| inclination: | 81.3035° |
| perigee height: | 946 km |
| apogee height: | 957 km |
| right ascension of ascending node: | 31.6408° |
| argument of perigee: | 250.0375° |
| revolutions per day: | 13.83431491 |
| mean anomaly at epoch: | 110.0006° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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