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 65145U 26145.46963964 +.00000000 +00000-0 +28625-3 0 00005
2 65145 51.8991 168.5741 0000384 77.2587 282.8418 14.79929078 08
| Epoch (UTC): | 25 May 2026 11:16:16 |
| Eccentricity: | 0.0000384 |
| inclination: | 51.8991° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 168.5741° |
| argument of perigee: | 77.2587° |
| revolutions per day: | 14.79929078 |
| mean anomaly at epoch: | 282.8418° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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