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 65332U 26145.44641587 +.00000000 +00000-0 +62887-3 0 00003
2 65332 53.1595 209.8516 0000936 59.5179 300.5915 15.31711869 09
| Epoch (UTC): | 25 May 2026 10:42:50 |
| Eccentricity: | 0.0000936 |
| inclination: | 53.1595° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 209.8516° |
| argument of perigee: | 59.5179° |
| revolutions per day: | 15.31711869 |
| mean anomaly at epoch: | 300.5915° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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