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 33496U 09002E 23083.60924349 .00001428 00000-0 23350-3 0 9990
2 33496 98.2708 320.1297 0006272 167.3696 192.7669 14.72437333760538
| Epoch (UTC): | 24 March 2023 14:37:18 |
| Eccentricity: | 0.0006272 |
| inclination: | 98.2708° |
| perigee height: | 649 km |
| apogee height: | 658 km |
| right ascension of ascending node: | 320.1297° |
| argument of perigee: | 167.3696° |
| revolutions per day: | 14.72437333 |
| mean anomaly at epoch: | 192.7669° |
| orbit number at epoch: | 76053 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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