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 68749U 26145.58335647 +.00000000 +00000-0 -10158-1 0 00003
2 68749 97.2850 9.3593 0001813 94.7899 166.5647 15.56869583 06
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001813 |
| inclination: | 97.2850° |
| perigee height: | 395 km |
| apogee height: | 398 km |
| right ascension of ascending node: | 9.3593° |
| argument of perigee: | 94.7899° |
| revolutions per day: | 15.56869583 |
| mean anomaly at epoch: | 166.5647° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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