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 68305U 26145.32223869 +.00000000 +00000-0 +12906-2 0 00008
2 68305 97.2815 271.1875 0000972 46.3739 313.7593 15.49198309 07
| Epoch (UTC): | 25 May 2026 07:44:01 |
| Eccentricity: | 0.0000972 |
| inclination: | 97.2815° |
| perigee height: | 418 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 271.1875° |
| argument of perigee: | 46.3739° |
| revolutions per day: | 15.49198309 |
| mean anomaly at epoch: | 313.7593° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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