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 47015U 99025FAR 24355.84055072 .00010908 00000-0 10512-2 0 9991
2 47015 98.7528 13.0302 0196868 171.4623 1.9436 14.79622036590893
| Epoch (UTC): | 20 December 2024 20:10:23 |
| Eccentricity: | 0.0196868 |
| inclination: | 98.7528° |
| perigee height: | 492 km |
| apogee height: | 768 km |
| right ascension of ascending node: | 13.0302° |
| argument of perigee: | 171.4623° |
| revolutions per day: | 14.79622036 |
| mean anomaly at epoch: | 1.9436° |
| orbit number at epoch: | 59089 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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