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 19046U 88032B 24282.50902866 .00025755 00000-0 14833-2 0 9990
2 19046 97.4623 261.3876 0029020 225.7089 134.1761 15.12034383973723
| Epoch (UTC): | 08 October 2024 12:13:00 |
| Eccentricity: | 0.0029020 |
| inclination: | 97.4623° |
| perigee height: | 510 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 261.3876° |
| argument of perigee: | 225.7089° |
| revolutions per day: | 15.12034383 |
| mean anomaly at epoch: | 134.1761° |
| orbit number at epoch: | 97372 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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