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 24259.19238480 .00010791 00000-0 12096-2 0 9993
2 33498 98.1132 175.2524 0011876 109.7772 250.4725 14.86963099843460
| Epoch (UTC): | 15 September 2024 04:37:02 |
| Eccentricity: | 0.0011876 |
| inclination: | 98.1132° |
| perigee height: | 599 km |
| apogee height: | 616 km |
| right ascension of ascending node: | 175.2524° |
| argument of perigee: | 109.7772° |
| revolutions per day: | 14.86963099 |
| mean anomaly at epoch: | 250.4725° |
| orbit number at epoch: | 84346 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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