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 65366U 26145.36795313 +.00000000 +00000-0 +84433-3 0 00009
2 65366 53.1580 172.1095 0001154 68.4926 291.6199 15.33564765 03
| Epoch (UTC): | 25 May 2026 08:49:51 |
| Eccentricity: | 0.0001154 |
| inclination: | 53.1580° |
| perigee height: | 464 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 172.1095° |
| argument of perigee: | 68.4926° |
| revolutions per day: | 15.33564765 |
| mean anomaly at epoch: | 291.6199° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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