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 66339U 26145.25061310 +.00000000 +00000-0 +57292-3 0 00004
2 66339 42.9987 140.1130 0001061 258.0998 101.9734 15.27595698 09
| Epoch (UTC): | 25 May 2026 06:00:52 |
| Eccentricity: | 0.0001061 |
| inclination: | 42.9987° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 140.1130° |
| argument of perigee: | 258.0998° |
| revolutions per day: | 15.27595698 |
| mean anomaly at epoch: | 101.9734° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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