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 24255.16049147 .00001968 00000-0 27745-3 0 9991
2 23343 97.7799 295.2735 0006620 180.2654 217.5865 14.78327976606974
| Epoch (UTC): | 11 September 2024 03:51:06 |
| Eccentricity: | 0.0006620 |
| inclination: | 97.7799° |
| perigee height: | 630 km |
| apogee height: | 639 km |
| right ascension of ascending node: | 295.2735° |
| argument of perigee: | 180.2654° |
| revolutions per day: | 14.78327976 |
| mean anomaly at epoch: | 217.5865° |
| orbit number at epoch: | 60697 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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