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 32788U 08021F 24285.38159480 .00379555 00000-0 13293-1 0 9991
2 32788 97.6033 266.7260 0008789 108.4037 251.8158 15.27798469895990
| Epoch (UTC): | 11 October 2024 09:09:29 |
| Eccentricity: | 0.0008789 |
| inclination: | 97.6033° |
| perigee height: | 476 km |
| apogee height: | 488 km |
| right ascension of ascending node: | 266.7260° |
| argument of perigee: | 108.4037° |
| revolutions per day: | 15.27798469 |
| mean anomaly at epoch: | 251.8158° |
| orbit number at epoch: | 89599 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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