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 66565U 26145.39792461 +.00000000 +00000-0 +61981-3 0 00008
2 66565 42.9967 273.6481 0000732 227.4325 132.6465 15.27590592 07
| Epoch (UTC): | 25 May 2026 09:33:00 |
| Eccentricity: | 0.0000732 |
| inclination: | 42.9967° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 273.6481° |
| argument of perigee: | 227.4325° |
| revolutions per day: | 15.27590592 |
| mean anomaly at epoch: | 132.6465° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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