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 47U 60007C 25134.16050758 .00000832 00000-0 20546-3 0 9994
2 47 66.6666 38.5449 0213112 70.2849 292.1108 14.44678374393592
| Epoch (UTC): | 14 May 2025 03:51:07 |
| Eccentricity: | 0.0213112 |
| inclination: | 66.6666° |
| perigee height: | 591 km |
| apogee height: | 895 km |
| right ascension of ascending node: | 38.5449° |
| argument of perigee: | 70.2849° |
| revolutions per day: | 14.44678374 |
| mean anomaly at epoch: | 292.1108° |
| orbit number at epoch: | 39359 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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