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 43679U 18084J 24358.04026582 .00013676 00000-0 91091-3 0 9995
2 43679 98.0670 170.1907 0002456 188.5260 171.5925 15.07234353335669
| Epoch (UTC): | 23 December 2024 00:57:58 |
| Eccentricity: | 0.0002456 |
| inclination: | 98.0670° |
| perigee height: | 543 km |
| apogee height: | 546 km |
| right ascension of ascending node: | 170.1907° |
| argument of perigee: | 188.5260° |
| revolutions per day: | 15.07234353 |
| mean anomaly at epoch: | 171.5925° |
| orbit number at epoch: | 33566 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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