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 65306U 26145.64190128 +.00000000 +00000-0 +29817-4 0 00003
2 65306 50.0100 286.6815 0000629 99.3965 260.6979 13.29320743 05
| Epoch (UTC): | 25 May 2026 15:24:20 |
| Eccentricity: | 0.0000629 |
| inclination: | 50.0100° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 286.6815° |
| argument of perigee: | 99.3965° |
| revolutions per day: | 13.29320743 |
| mean anomaly at epoch: | 260.6979° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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