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 24277.19487269 .00000335 00000-0 18160-3 0 9999
2 19120 71.0126 93.2512 0019967 58.3998 301.9073 14.19459962884506
| Epoch (UTC): | 03 October 2024 04:40:37 |
| Eccentricity: | 0.0019967 |
| inclination: | 71.0126° |
| perigee height: | 813 km |
| apogee height: | 841 km |
| right ascension of ascending node: | 93.2512° |
| argument of perigee: | 58.3998° |
| revolutions per day: | 14.19459962 |
| mean anomaly at epoch: | 301.9073° |
| orbit number at epoch: | 88450 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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