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 24357.59715068 .00001409 00000-0 32717-3 0 9993
2 00047 66.6656 61.1770 0221250 177.6463 182.5741 14.44281382372564
| Epoch (UTC): | 22 December 2024 14:19:53 |
| Eccentricity: | 0.0221250 |
| inclination: | 66.6656° |
| perigee height: | 587 km |
| apogee height: | 902 km |
| right ascension of ascending node: | 61.1770° |
| argument of perigee: | 177.6463° |
| revolutions per day: | 14.44281382 |
| mean anomaly at epoch: | 182.5741° |
| orbit number at epoch: | 37256 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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