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 65937U 26145.36055904 +.00000000 +00000-0 +32513-3 0 00000
2 65937 53.1566 169.7684 0001037 62.4026 297.7080 15.30201891 03
| Epoch (UTC): | 25 May 2026 08:39:12 |
| Eccentricity: | 0.0001037 |
| inclination: | 53.1566° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 169.7684° |
| argument of perigee: | 62.4026° |
| revolutions per day: | 15.30201891 |
| mean anomaly at epoch: | 297.7080° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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