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 32785U 08021C 25348.23224500 .00007023 00000-0 47205-3 0 9999
2 32785 97.8077 321.3419 0007894 304.4990 55.5491 15.07067785957315
| Epoch (UTC): | 14 December 2025 05:34:25 |
| Eccentricity: | 0.0007894 |
| inclination: | 97.8077° |
| perigee height: | 540 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 321.3419° |
| argument of perigee: | 304.4990° |
| revolutions per day: | 15.07067785 |
| mean anomaly at epoch: | 55.5491° |
| orbit number at epoch: | 95731 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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