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 65225U 26145.40903939 +.00000000 +00000-0 +53214-3 0 00006
2 65225 53.1590 155.8629 0001299 76.0554 284.0593 15.34401094 01
| Epoch (UTC): | 25 May 2026 09:49:01 |
| Eccentricity: | 0.0001299 |
| inclination: | 53.1590° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 155.8629° |
| argument of perigee: | 76.0554° |
| revolutions per day: | 15.34401094 |
| mean anomaly at epoch: | 284.0593° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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