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 32432U 99025DAU 25320.84691514 .00013157 00000-0 26748-2 0 9995
2 32432 98.1746 357.7041 0174998 25.7197 335.2573 14.51947171703195
| Epoch (UTC): | 16 November 2025 20:19:33 |
| Eccentricity: | 0.0174998 |
| inclination: | 98.1746° |
| perigee height: | 595 km |
| apogee height: | 843 km |
| right ascension of ascending node: | 357.7041° |
| argument of perigee: | 25.7197° |
| revolutions per day: | 14.51947171 |
| mean anomaly at epoch: | 335.2573° |
| orbit number at epoch: | 70319 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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