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 68805U 26145.33335647 +.00000000 +00000-0 -27578-3 0 00005
2 68805 97.2850 351.9828 0001556 85.8905 49.1769 15.75198848 00
| Epoch (UTC): | 25 May 2026 08:00:01 |
| Eccentricity: | 0.0001556 |
| inclination: | 97.2850° |
| perigee height: | 343 km |
| apogee height: | 345 km |
| right ascension of ascending node: | 351.9828° |
| argument of perigee: | 85.8905° |
| revolutions per day: | 15.75198848 |
| mean anomaly at epoch: | 49.1769° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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