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 25198.47365817 .00000108 00000-0 47813-4 0 9990
2 23432 74.0332 297.5252 0004866 162.1577 282.0285 14.34274939599398
| Epoch (UTC): | 17 July 2025 11:22:04 |
| Eccentricity: | 0.0004866 |
| inclination: | 74.0332° |
| perigee height: | 774 km |
| apogee height: | 781 km |
| right ascension of ascending node: | 297.5252° |
| argument of perigee: | 162.1577° |
| revolutions per day: | 14.34274939 |
| mean anomaly at epoch: | 282.0285° |
| orbit number at epoch: | 59939 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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