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 26022.31707450 +.00000000 +00000-0 +13084-3 0 00006
2 23343 97.7166 55.0016 0007075 24.3203 346.1916 14.79345160 03
| Epoch (UTC): | 22 January 2026 07:36:35 |
| Eccentricity: | 0.0007075 |
| inclination: | 97.7166° |
| perigee height: | 626 km |
| apogee height: | 636 km |
| right ascension of ascending node: | 55.0016° |
| argument of perigee: | 24.3203° |
| revolutions per day: | 14.79345160 |
| mean anomaly at epoch: | 346.1916° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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