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 is defined by the following mean orbital elements,
1 23432U 26088.24382910 +.00000000 +00000-0 +89675-4 0 00009
2 23432 74.0331 190.9598 0005894 333.4188 52.3470 14.34432121 07
| Epoch (UTC): | 29 March 2026 05:51:06 |
| Eccentricity: | 0.0005894 |
| inclination: | 74.0331° |
| perigee height: | 773 km |
| apogee height: | 781 km |
| right ascension of ascending node: | 190.9598° |
| argument of perigee: | 333.4188° |
| revolutions per day: | 14.34432121 |
| mean anomaly at epoch: | 52.3470° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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