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 25343.00311625 .00000782 00000-0 18698-3 0 9991
2 47 66.6635 197.6636 0226524 277.3282 80.2130 14.45030629423327
| Epoch (UTC): | 09 December 2025 00:04:29 |
| Eccentricity: | 0.0226524 |
| inclination: | 66.6635° |
| perigee height: | 580 km |
| apogee height: | 903 km |
| right ascension of ascending node: | 197.6636° |
| argument of perigee: | 277.3282° |
| revolutions per day: | 14.45030629 |
| mean anomaly at epoch: | 80.2130° |
| orbit number at epoch: | 42332 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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