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 68606U 26145.50003470 +.00000000 +00000-0 -25090-1 0 00004
2 68606 97.2847 345.0661 0001868 71.9967 95.7928 15.60725604 08
| Epoch (UTC): | 25 May 2026 12:00:02 |
| Eccentricity: | 0.0001868 |
| inclination: | 97.2847° |
| perigee height: | 384 km |
| apogee height: | 387 km |
| right ascension of ascending node: | 345.0661° |
| argument of perigee: | 71.9967° |
| revolutions per day: | 15.60725604 |
| mean anomaly at epoch: | 95.7928° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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