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 66306U 26145.32111389 +.00000000 +00000-0 +58266-3 0 00000
2 66306 45.4032 237.5939 0014256 292.6280 67.3101 15.26593972 03
| Epoch (UTC): | 25 May 2026 07:42:24 |
| Eccentricity: | 0.0014256 |
| inclination: | 45.4032° |
| perigee height: | 476 km |
| apogee height: | 496 km |
| right ascension of ascending node: | 237.5939° |
| argument of perigee: | 292.6280° |
| revolutions per day: | 15.26593972 |
| mean anomaly at epoch: | 67.3101° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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