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 25198.47244408 .00000263 00000-0 80927-4 0 9993
2 47 66.6629 225.8694 0217191 21.8471 339.1722 14.44746298402886
| Epoch (UTC): | 17 July 2025 11:20:19 |
| Eccentricity: | 0.0217191 |
| inclination: | 66.6629° |
| perigee height: | 588 km |
| apogee height: | 897 km |
| right ascension of ascending node: | 225.8694° |
| argument of perigee: | 21.8471° |
| revolutions per day: | 14.44746298 |
| mean anomaly at epoch: | 339.1722° |
| orbit number at epoch: | 40288 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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