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 24260.89368955 .00012311 00000-0 10304-2 0 9991
2 32785 97.7628 225.5968 0011287 28.7099 331.4743 14.98549323889274
| Epoch (UTC): | 16 September 2024 21:26:54 |
| Eccentricity: | 0.0011287 |
| inclination: | 97.7628° |
| perigee height: | 563 km |
| apogee height: | 579 km |
| right ascension of ascending node: | 225.5968° |
| argument of perigee: | 28.7099° |
| revolutions per day: | 14.98549323 |
| mean anomaly at epoch: | 331.4743° |
| orbit number at epoch: | 88927 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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