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 67226U 26144.66615456 +.00000000 +00000-0 +00000-0 0 00002
2 67226 5.6415 297.6108 0004741 156.0166 203.9581 1.00269665 03
| Epoch (UTC): | 24 May 2026 15:59:15 |
| Eccentricity: | 0.0004741 |
| inclination: | 5.6415° |
| perigee height: | 35767 km |
| apogee height: | 35807 km |
| right ascension of ascending node: | 297.6108° |
| argument of perigee: | 156.0166° |
| revolutions per day: | 1.00269665 |
| mean anomaly at epoch: | 203.9581° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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