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 24281.85312979 .00002647 00000-0 36976-3 0 9993
2 23343 97.7754 321.0626 0008116 103.6751 69.4445 14.78423794610913
| Epoch (UTC): | 07 October 2024 20:28:30 |
| Eccentricity: | 0.0008116 |
| inclination: | 97.7754° |
| perigee height: | 628 km |
| apogee height: | 640 km |
| right ascension of ascending node: | 321.0626° |
| argument of perigee: | 103.6751° |
| revolutions per day: | 14.78423794 |
| mean anomaly at epoch: | 69.4445° |
| orbit number at epoch: | 61091 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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