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 24340.49546683 .00009040 00000-0 96846-3 0 9995
2 33498 98.1188 258.4396 0008273 199.7407 160.3490 14.88889024855135
| Epoch (UTC): | 05 December 2024 11:53:28 |
| Eccentricity: | 0.0008273 |
| inclination: | 98.1188° |
| perigee height: | 595 km |
| apogee height: | 607 km |
| right ascension of ascending node: | 258.4396° |
| argument of perigee: | 199.7407° |
| revolutions per day: | 14.88889024 |
| mean anomaly at epoch: | 160.3490° |
| orbit number at epoch: | 85513 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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