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 68669U 26145.59922294 +.00000000 +00000-0 +87934-3 0 00002
2 68669 97.2866 17.1551 0002031 85.1230 275.0244 15.33455094 03
| Epoch (UTC): | 25 May 2026 14:22:52 |
| Eccentricity: | 0.0002031 |
| inclination: | 97.2866° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 17.1551° |
| argument of perigee: | 85.1230° |
| revolutions per day: | 15.33455094 |
| mean anomaly at epoch: | 275.0244° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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