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 27751U 92093JN 23341.88763423 .00033743 00000-0 41105-2 0 9992
2 27751 71.1524 306.5568 0028324 233.3154 126.5403 14.82960379527191
| Epoch (UTC): | 07 December 2023 21:18:11 |
| Eccentricity: | 0.0028324 |
| inclination: | 71.1524° |
| perigee height: | 600 km |
| apogee height: | 640 km |
| right ascension of ascending node: | 306.5568° |
| argument of perigee: | 233.3154° |
| revolutions per day: | 14.82960379 |
| mean anomaly at epoch: | 126.5403° |
| orbit number at epoch: | 52719 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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