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 36288U 10001B 23333.36305801 .00004422 00000-0 18216-2 0 9991
2 36288 20.3725 10.2879 7040935 103.2230 337.6355 2.57462979123643
| Epoch (UTC): | 29 November 2023 08:42:48 |
| Eccentricity: | 0.7040935 |
| inclination: | 20.3725° |
| perigee height: | 276 km |
| apogee height: | 31941 km |
| right ascension of ascending node: | 10.2879° |
| argument of perigee: | 103.2230° |
| revolutions per day: | 2.57462979 |
| mean anomaly at epoch: | 337.6355° |
| orbit number at epoch: | 12364 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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