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 66983U 26145.50499669 +.00000000 +00000-0 +52809-3 0 00008
2 66983 43.0002 309.7834 0000471 317.6908 42.3907 15.27594579 02
| Epoch (UTC): | 25 May 2026 12:07:11 |
| Eccentricity: | 0.0000471 |
| inclination: | 43.0002° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 309.7834° |
| argument of perigee: | 317.6908° |
| revolutions per day: | 15.27594579 |
| mean anomaly at epoch: | 42.3907° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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