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 26064.67778605 +.00000000 +00000-0 +99908-4 0 00001
2 23343 97.7114 95.6579 0005501 225.8356 249.4636 14.79402865 09
| Epoch (UTC): | 05 March 2026 16:16:00 |
| Eccentricity: | 0.0005501 |
| inclination: | 97.7114° |
| perigee height: | 627 km |
| apogee height: | 635 km |
| right ascension of ascending node: | 95.6579° |
| argument of perigee: | 225.8356° |
| revolutions per day: | 14.79402865 |
| mean anomaly at epoch: | 249.4636° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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