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 data is extracted from the following two-line orbital elements,
1 23343U 94074B 24357.70532424 .00000986 00000-0 14127-3 0 9998
2 23343 97.7640 34.2791 0005851 208.9348 264.9233 14.78668741621919
| Epoch (UTC): | 22 December 2024 16:55:40 |
| Eccentricity: | 0.0005851 |
| inclination: | 97.7640° |
| perigee height: | 629 km |
| apogee height: | 637 km |
| right ascension of ascending node: | 34.2791° |
| argument of perigee: | 208.9348° |
| revolutions per day: | 14.78668741 |
| mean anomaly at epoch: | 264.9233° |
| orbit number at epoch: | 62191 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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