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 66599U 26145.23933692 +.00000000 +00000-0 +83651-3 0 00009
2 66599 42.9986 343.8226 0001923 276.7893 83.2740 15.27599300 05
| Epoch (UTC): | 25 May 2026 05:44:38 |
| Eccentricity: | 0.0001923 |
| inclination: | 42.9986° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 343.8226° |
| argument of perigee: | 276.7893° |
| revolutions per day: | 15.27599300 |
| mean anomaly at epoch: | 83.2740° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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