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 32791U 08021J 25191.46684908 .00006531 00000-0 31272-3 0 9999
2 32791 97.7282 172.2113 0005614 74.7249 285.4605 15.19293008935189
| Epoch (UTC): | 10 July 2025 11:12:15 |
| Eccentricity: | 0.0005614 |
| inclination: | 97.7282° |
| perigee height: | 504 km |
| apogee height: | 512 km |
| right ascension of ascending node: | 172.2113° |
| argument of perigee: | 74.7249° |
| revolutions per day: | 15.19293008 |
| mean anomaly at epoch: | 285.4605° |
| orbit number at epoch: | 93518 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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