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 25133.86510319 .00005982 00000-0 43524-3 0 9998
2 32785 97.7838 104.8385 0008586 309.0719 50.9742 15.04163175925066
| Epoch (UTC): | 13 May 2025 20:45:44 |
| Eccentricity: | 0.0008586 |
| inclination: | 97.7838° |
| perigee height: | 548 km |
| apogee height: | 560 km |
| right ascension of ascending node: | 104.8385° |
| argument of perigee: | 309.0719° |
| revolutions per day: | 15.04163175 |
| mean anomaly at epoch: | 50.9742° |
| orbit number at epoch: | 92506 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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