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 25112.45478701 .00021353 00000-0 10730-2 0 9997
2 32791 97.7257 91.4778 0003715 18.6009 341.5359 15.17283268923273
| Epoch (UTC): | 22 April 2025 10:54:53 |
| Eccentricity: | 0.0003715 |
| inclination: | 97.7257° |
| perigee height: | 511 km |
| apogee height: | 516 km |
| right ascension of ascending node: | 91.4778° |
| argument of perigee: | 18.6009° |
| revolutions per day: | 15.17283268 |
| mean anomaly at epoch: | 341.5359° |
| orbit number at epoch: | 92327 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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