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 35433U 93036AKB 24353.09115266 .00001190 00000-0 43410-3 0 9992
2 35433 74.0372 277.0215 0025397 61.2589 312.1893 14.33971079814244
| Epoch (UTC): | 18 December 2024 02:11:15 |
| Eccentricity: | 0.0025397 |
| inclination: | 74.0372° |
| perigee height: | 760 km |
| apogee height: | 796 km |
| right ascension of ascending node: | 277.0215° |
| argument of perigee: | 61.2589° |
| revolutions per day: | 14.33971079 |
| mean anomaly at epoch: | 312.1893° |
| orbit number at epoch: | 81424 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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