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 19120U 88039B 24287.48352098 .00000161 00000-0 99228-4 0 9995
2 19120 71.0140 71.4989 0020387 41.2124 319.0536 14.19468683885693
| Epoch (UTC): | 13 October 2024 11:36:16 |
| Eccentricity: | 0.0020387 |
| inclination: | 71.0140° |
| perigee height: | 812 km |
| apogee height: | 842 km |
| right ascension of ascending node: | 71.4989° |
| argument of perigee: | 41.2124° |
| revolutions per day: | 14.19468683 |
| mean anomaly at epoch: | 319.0536° |
| orbit number at epoch: | 88569 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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