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 24280.92980320 .00000538 00000-0 27754-3 0 9994
2 19120 71.0134 85.3546 0020001 52.0055 308.2872 14.19463082885034
| Epoch (UTC): | 06 October 2024 22:18:54 |
| Eccentricity: | 0.0020001 |
| inclination: | 71.0134° |
| perigee height: | 813 km |
| apogee height: | 841 km |
| right ascension of ascending node: | 85.3546° |
| argument of perigee: | 52.0055° |
| revolutions per day: | 14.19463082 |
| mean anomaly at epoch: | 308.2872° |
| orbit number at epoch: | 88503 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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