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 33843U 93036CL 23337.09079874 .00025823 00000-0 30635-2 0 9993
2 33843 73.9796 298.4443 0150796 269.0147 89.3748 14.76533331782502
| Epoch (UTC): | 03 December 2023 02:10:45 |
| Eccentricity: | 0.0150796 |
| inclination: | 73.9796° |
| perigee height: | 534 km |
| apogee height: | 746 km |
| right ascension of ascending node: | 298.4443° |
| argument of perigee: | 269.0147° |
| revolutions per day: | 14.76533331 |
| mean anomaly at epoch: | 89.3748° |
| orbit number at epoch: | 78250 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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