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 66604U 26145.27774153 +.00000000 +00000-0 +55649-3 0 00001
2 66604 43.0021 343.2529 0001807 276.5672 83.4974 15.27590999 04
| Epoch (UTC): | 25 May 2026 06:39:56 |
| Eccentricity: | 0.0001807 |
| inclination: | 43.0021° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 343.2529° |
| argument of perigee: | 276.5672° |
| revolutions per day: | 15.27590999 |
| mean anomaly at epoch: | 83.4974° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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