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 66813U 26145.39358752 +.00000000 +00000-0 +68766-3 0 00003
2 66813 42.9978 40.8625 0000285 329.4693 30.6142 15.27582748 06
| Epoch (UTC): | 25 May 2026 09:26:45 |
| Eccentricity: | 0.0000285 |
| inclination: | 42.9978° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 40.8625° |
| argument of perigee: | 329.4693° |
| revolutions per day: | 15.27582748 |
| mean anomaly at epoch: | 30.6142° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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