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 68611U 26145.58335647 +.00000000 +00000-0 -35877-1 0 00006
2 68611 97.2838 345.1862 0001461 72.8416 290.5513 15.61135520 04
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001461 |
| inclination: | 97.2838° |
| perigee height: | 383 km |
| apogee height: | 385 km |
| right ascension of ascending node: | 345.1862° |
| argument of perigee: | 72.8416° |
| revolutions per day: | 15.61135520 |
| mean anomaly at epoch: | 290.5513° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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