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 68816U 26145.55589112 +.00000000 +00000-0 +13984-2 0 00003
2 68816 97.2859 352.2327 0001834 89.8300 270.3175 15.75266219 08
| Epoch (UTC): | 25 May 2026 13:20:28 |
| Eccentricity: | 0.0001834 |
| inclination: | 97.2859° |
| perigee height: | 343 km |
| apogee height: | 345 km |
| right ascension of ascending node: | 352.2327° |
| argument of perigee: | 89.8300° |
| revolutions per day: | 15.75266219 |
| mean anomaly at epoch: | 270.3175° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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