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 68895U 26145.58335647 +.00000000 +00000-0 -56058-1 0 00004
2 68895 97.2853 341.3341 0001592 76.6344 9.5807 15.43618445 08
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001592 |
| inclination: | 97.2853° |
| perigee height: | 434 km |
| apogee height: | 437 km |
| right ascension of ascending node: | 341.3341° |
| argument of perigee: | 76.6344° |
| revolutions per day: | 15.43618445 |
| mean anomaly at epoch: | 9.5807° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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