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 68214U 26145.37733828 +.00000000 +00000-0 +62813-3 0 00006
2 68214 97.2861 20.8626 0001994 88.4105 271.7366 15.33431851 05
| Epoch (UTC): | 25 May 2026 09:03:22 |
| Eccentricity: | 0.0001994 |
| inclination: | 97.2861° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 20.8626° |
| argument of perigee: | 88.4105° |
| revolutions per day: | 15.33431851 |
| mean anomaly at epoch: | 271.7366° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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