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 65307U 26145.62526769 +.00000000 +00000-0 +50412-4 0 00001
2 65307 50.0092 286.5784 0000604 99.5475 260.5466 13.29322293 03
| Epoch (UTC): | 25 May 2026 15:00:23 |
| Eccentricity: | 0.0000604 |
| inclination: | 50.0092° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 286.5784° |
| argument of perigee: | 99.5475° |
| revolutions per day: | 13.29322293 |
| mean anomaly at epoch: | 260.5466° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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