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 68306U 26145.32972463 +.00000000 +00000-0 +97126-3 0 00008
2 68306 97.2854 271.6400 0001365 9.0012 351.1277 15.75203183 08
| Epoch (UTC): | 25 May 2026 07:54:48 |
| Eccentricity: | 0.0001365 |
| inclination: | 97.2854° |
| perigee height: | 343 km |
| apogee height: | 345 km |
| right ascension of ascending node: | 271.6400° |
| argument of perigee: | 9.0012° |
| revolutions per day: | 15.75203183 |
| mean anomaly at epoch: | 351.1277° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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