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 23432U 94083B 25199.74427767 .00000108 00000-0 47615-4 0 9994
2 23432 74.0331 295.1988 0004819 159.3633 2.8950 14.34275368599345
| Epoch (UTC): | 18 July 2025 17:51:45 |
| Eccentricity: | 0.0004819 |
| inclination: | 74.0331° |
| perigee height: | 774 km |
| apogee height: | 781 km |
| right ascension of ascending node: | 295.1988° |
| argument of perigee: | 159.3633° |
| revolutions per day: | 14.34275368 |
| mean anomaly at epoch: | 2.8950° |
| orbit number at epoch: | 59934 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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