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 00047U 60007C 25339.05800004 .00001051 00000-0 24302-3 0 9994
2 00047 66.6636 208.2630 0226514 280.1351 77.4275 14.45023612422757
| Epoch (UTC): | 05 December 2025 01:23:31 |
| Eccentricity: | 0.0226514 |
| inclination: | 66.6636° |
| perigee height: | 580 km |
| apogee height: | 903 km |
| right ascension of ascending node: | 208.2630° |
| argument of perigee: | 280.1351° |
| revolutions per day: | 14.45023612 |
| mean anomaly at epoch: | 77.4275° |
| orbit number at epoch: | 42275 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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