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 68666U 26145.21586722 +.00000000 +00000-0 +56426-3 0 00002
2 68666 97.2859 16.7578 0002157 95.0904 265.0585 15.33452559 03
| Epoch (UTC): | 25 May 2026 05:10:50 |
| Eccentricity: | 0.0002157 |
| inclination: | 97.2859° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 16.7578° |
| argument of perigee: | 95.0904° |
| revolutions per day: | 15.33452559 |
| mean anomaly at epoch: | 265.0585° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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