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 68008U 26145.52103618 +.00000000 +00000-0 +68555-3 0 00001
2 68008 43.0030 335.0332 0001627 264.4926 95.5740 15.27593834 09
| Epoch (UTC): | 25 May 2026 12:30:17 |
| Eccentricity: | 0.0001627 |
| inclination: | 43.0030° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 335.0332° |
| argument of perigee: | 264.4926° |
| revolutions per day: | 15.27593834 |
| mean anomaly at epoch: | 95.5740° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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