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 23343U 26069.54841931 +.00000000 +00000-0 +84850-4 0 00005
2 23343 97.7109 100.3313 0005866 207.1181 272.6344 14.79409106 05
| Epoch (UTC): | 10 March 2026 13:09:43 |
| Eccentricity: | 0.0005866 |
| inclination: | 97.7109° |
| perigee height: | 627 km |
| apogee height: | 635 km |
| right ascension of ascending node: | 100.3313° |
| argument of perigee: | 207.1181° |
| revolutions per day: | 14.79409106 |
| mean anomaly at epoch: | 272.6344° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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