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 26086.87297265 +.00000000 +00000-0 +67958-4 0 00005
2 23343 97.7083 116.9524 0007219 151.0753 21.2144 14.79427896 01
| Epoch (UTC): | 27 March 2026 20:57:04 |
| Eccentricity: | 0.0007219 |
| inclination: | 97.7083° |
| perigee height: | 626 km |
| apogee height: | 636 km |
| right ascension of ascending node: | 116.9524° |
| argument of perigee: | 151.0753° |
| revolutions per day: | 14.79427896 |
| mean anomaly at epoch: | 21.2144° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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