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 43669U 18083H 24130.99921043 .13914420 25146-5 50688-3 0 9992
2 43669 97.2952 170.3552 0012886 250.8284 109.1623 16.43032312307806
| Epoch (UTC): | 09 May 2024 23:58:51 |
| Eccentricity: | 0.0012886 |
| inclination: | 97.2952° |
| perigee height: | 149 km |
| apogee height: | 166 km |
| right ascension of ascending node: | 170.3552° |
| argument of perigee: | 250.8284° |
| revolutions per day: | 16.43032312 |
| mean anomaly at epoch: | 109.1623° |
| orbit number at epoch: | 30780 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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