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 68389U 26145.58335647 +.00000000 +00000-0 -10121-2 0 00004
2 68389 97.2926 288.1907 0000606 126.2144 204.9560 15.33441658 04
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0000606 |
| inclination: | 97.2926° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 288.1907° |
| argument of perigee: | 126.2144° |
| revolutions per day: | 15.33441658 |
| mean anomaly at epoch: | 204.9560° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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