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 66964U 26145.45245764 +.00000000 +00000-0 +79441-3 0 00007
2 66964 43.0002 310.2592 0001423 270.5869 89.4819 15.27602604 03
| Epoch (UTC): | 25 May 2026 10:51:32 |
| Eccentricity: | 0.0001423 |
| inclination: | 43.0002° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 310.2592° |
| argument of perigee: | 270.5869° |
| revolutions per day: | 15.27602604 |
| mean anomaly at epoch: | 89.4819° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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