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 26049.66238816 +.00000000 +00000-0 +67951-4 0 00001
2 23343 97.7135 81.2484 0005161 287.1104 187.8753 14.79384369 05
| Epoch (UTC): | 18 February 2026 15:53:50 |
| Eccentricity: | 0.0005161 |
| inclination: | 97.7135° |
| perigee height: | 628 km |
| apogee height: | 635 km |
| right ascension of ascending node: | 81.2484° |
| argument of perigee: | 287.1104° |
| revolutions per day: | 14.79384369 |
| mean anomaly at epoch: | 187.8753° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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