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 68006U 26145.52874753 +.00000000 +00000-0 +59319-3 0 00002
2 68006 43.0032 335.0979 0001470 271.1749 88.8935 15.27591030 07
| Epoch (UTC): | 25 May 2026 12:41:23 |
| Eccentricity: | 0.0001470 |
| inclination: | 43.0032° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 335.0979° |
| argument of perigee: | 271.1749° |
| revolutions per day: | 15.27591030 |
| mean anomaly at epoch: | 88.8935° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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