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 68583U 26145.58335647 +.00000000 +00000-0 -33407-1 0 00001
2 68583 51.8777 285.9994 0002783 293.6872 164.3170 15.34218958 08
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0002783 |
| inclination: | 51.8777° |
| perigee height: | 461 km |
| apogee height: | 465 km |
| right ascension of ascending node: | 285.9994° |
| argument of perigee: | 293.6872° |
| revolutions per day: | 15.34218958 |
| mean anomaly at epoch: | 164.3170° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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