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 68917U 26145.50993852 +.00000000 +00000-0 +88698-3 0 00005
2 68917 97.2869 341.2407 0000971 67.1584 292.9769 15.49212150 07
| Epoch (UTC): | 25 May 2026 12:14:18 |
| Eccentricity: | 0.0000971 |
| inclination: | 97.2869° |
| perigee height: | 418 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 341.2407° |
| argument of perigee: | 67.1584° |
| revolutions per day: | 15.49212150 |
| mean anomaly at epoch: | 292.9769° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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