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 23029.73754492 .00003405 00000-0 35158-3 0 9990
2 32785 97.6885 358.9514 0011905 194.8723 165.2146 14.90765720800188
| Epoch (UTC): | 29 January 2023 17:42:03 |
| Eccentricity: | 0.0011905 |
| inclination: | 97.6885° |
| perigee height: | 587 km |
| apogee height: | 604 km |
| right ascension of ascending node: | 358.9514° |
| argument of perigee: | 194.8723° |
| revolutions per day: | 14.90765720 |
| mean anomaly at epoch: | 165.2146° |
| orbit number at epoch: | 80018 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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