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 68375U 26162.71759843 +.00000000 +00000-0 -24546-2 0 00007
2 68375 82.2934 18.8333 0006661 258.1678 101.8838 15.74120508 03
| Epoch (UTC): | 11 June 2026 17:13:20 |
| Eccentricity: | 0.0006661 |
| inclination: | 82.2934° |
| perigee height: | 343 km |
| apogee height: | 352 km |
| right ascension of ascending node: | 18.8333° |
| argument of perigee: | 258.1678° |
| revolutions per day: | 15.74120508 |
| mean anomaly at epoch: | 101.8838° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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