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 65996U 26145.24373185 +.00000000 +00000-0 +40134-4 0 00005
2 65996 49.9994 258.1869 0000928 150.9298 209.1625 13.29328354 08
| Epoch (UTC): | 25 May 2026 05:50:58 |
| Eccentricity: | 0.0000928 |
| inclination: | 49.9994° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 258.1869° |
| argument of perigee: | 150.9298° |
| revolutions per day: | 13.29328354 |
| mean anomaly at epoch: | 209.1625° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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