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 33498U 09002G 24262.35504939 .00010588 00000-0 11851-2 0 9992
2 33498 98.1136 178.4827 0011877 101.0444 259.2108 14.87028800843518
| Epoch (UTC): | 18 September 2024 08:31:16 |
| Eccentricity: | 0.0011877 |
| inclination: | 98.1136° |
| perigee height: | 599 km |
| apogee height: | 615 km |
| right ascension of ascending node: | 178.4827° |
| argument of perigee: | 101.0444° |
| revolutions per day: | 14.87028800 |
| mean anomaly at epoch: | 259.2108° |
| orbit number at epoch: | 84351 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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