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 65311U 26145.61679632 +.00000000 +00000-0 +45180-4 0 00009
2 65311 50.0046 287.0912 0000631 102.5032 257.5911 13.29318756 00
| Epoch (UTC): | 25 May 2026 14:48:11 |
| Eccentricity: | 0.0000631 |
| inclination: | 50.0046° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 287.0912° |
| argument of perigee: | 102.5032° |
| revolutions per day: | 13.29318756 |
| mean anomaly at epoch: | 257.5911° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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