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 65362U 26145.45217389 +.00000000 +00000-0 +21333-3 0 00007
2 65362 53.1597 171.2147 0001187 88.3795 271.7344 15.34395691 08
| Epoch (UTC): | 25 May 2026 10:51:07 |
| Eccentricity: | 0.0001187 |
| inclination: | 53.1597° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 171.2147° |
| argument of perigee: | 88.3795° |
| revolutions per day: | 15.34395691 |
| mean anomaly at epoch: | 271.7344° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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