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 25197.02615992 .00000095 00000-0 43209-4 0 9992
2 23432 74.0333 300.1755 0004920 165.0911 8.0978 14.34274438599189
| Epoch (UTC): | 16 July 2025 00:37:40 |
| Eccentricity: | 0.0004920 |
| inclination: | 74.0333° |
| perigee height: | 774 km |
| apogee height: | 781 km |
| right ascension of ascending node: | 300.1755° |
| argument of perigee: | 165.0911° |
| revolutions per day: | 14.34274438 |
| mean anomaly at epoch: | 8.0978° |
| orbit number at epoch: | 59918 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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