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 65473U 26144.81301794 +.00000000 +00000-0 +14237-2 0 00007
2 65473 53.1586 264.2332 0001145 88.3673 271.7460 15.34458945 08
| Epoch (UTC): | 24 May 2026 19:30:44 |
| Eccentricity: | 0.0001145 |
| inclination: | 53.1586° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 264.2332° |
| argument of perigee: | 88.3673° |
| revolutions per day: | 15.34458945 |
| mean anomaly at epoch: | 271.7460° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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