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 65926U 26145.44686683 +.00000000 +00000-0 +21434-3 0 00001
2 65926 53.1584 168.8849 0000729 74.8264 285.2817 15.30197322 05
| Epoch (UTC): | 25 May 2026 10:43:29 |
| Eccentricity: | 0.0000729 |
| inclination: | 53.1584° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 168.8849° |
| argument of perigee: | 74.8264° |
| revolutions per day: | 15.30197322 |
| mean anomaly at epoch: | 285.2817° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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