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 41147U 00055CE 24358.34738819 .00010334 00000-0 57647-2 0 9994
2 41147 98.9504 28.9614 0074743 154.7376 205.7478 14.09628026462162
| Epoch (UTC): | 23 December 2024 08:20:14 |
| Eccentricity: | 0.0074743 |
| inclination: | 98.9504° |
| perigee height: | 806 km |
| apogee height: | 915 km |
| right ascension of ascending node: | 28.9614° |
| argument of perigee: | 154.7376° |
| revolutions per day: | 14.09628026 |
| mean anomaly at epoch: | 205.7478° |
| orbit number at epoch: | 46216 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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