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 66803U 26145.43727402 +.00000000 +00000-0 +58724-3 0 00002
2 66803 43.0032 41.2000 0001434 266.6140 93.4547 15.27589287 07
| Epoch (UTC): | 25 May 2026 10:29:40 |
| Eccentricity: | 0.0001434 |
| inclination: | 43.0032° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 41.2000° |
| argument of perigee: | 266.6140° |
| revolutions per day: | 15.27589287 |
| mean anomaly at epoch: | 93.4547° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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