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 65471U 26145.63468094 +.00000000 +00000-0 +21093-2 0 00001
2 65471 53.1593 260.8232 0004454 72.0296 288.1190 15.30424157 08
| Epoch (UTC): | 25 May 2026 15:13:56 |
| Eccentricity: | 0.0004454 |
| inclination: | 53.1593° |
| perigee height: | 471 km |
| apogee height: | 478 km |
| right ascension of ascending node: | 260.8232° |
| argument of perigee: | 72.0296° |
| revolutions per day: | 15.30424157 |
| mean anomaly at epoch: | 288.1190° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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