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 66577U 26145.41462494 +.00000000 +00000-0 +61604-3 0 00006
2 66577 42.9998 273.7727 0001188 232.8878 127.1865 15.27591149 09
| Epoch (UTC): | 25 May 2026 09:57:03 |
| Eccentricity: | 0.0001188 |
| inclination: | 42.9998° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 273.7727° |
| argument of perigee: | 232.8878° |
| revolutions per day: | 15.27591149 |
| mean anomaly at epoch: | 127.1865° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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