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 66799U 26145.39744179 +.00000000 +00000-0 +52493-3 0 00008
2 66799 43.0019 40.8910 0000910 4.6740 355.4121 15.27593855 00
| Epoch (UTC): | 25 May 2026 09:32:18 |
| Eccentricity: | 0.0000910 |
| inclination: | 43.0019° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 40.8910° |
| argument of perigee: | 4.6740° |
| revolutions per day: | 15.27593855 |
| mean anomaly at epoch: | 355.4121° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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