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 00047U 60007C 24250.59036300 .00002889 00000-0 63619-3 0 9998
2 00047 66.6686 348.2163 0230463 254.6888 102.8642 14.43808214357112
| Epoch (UTC): | 06 September 2024 14:10:07 |
| Eccentricity: | 0.0230463 |
| inclination: | 66.6686° |
| perigee height: | 582 km |
| apogee height: | 910 km |
| right ascension of ascending node: | 348.2163° |
| argument of perigee: | 254.6888° |
| revolutions per day: | 14.43808214 |
| mean anomaly at epoch: | 102.8642° |
| orbit number at epoch: | 35711 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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