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 33499U 09002H 24259.86908750 .00005736 00000-0 77402-3 0 9998
2 33499 98.1281 162.5269 0008010 186.8038 173.3066 14.79484560841527
| Epoch (UTC): | 15 September 2024 20:51:29 |
| Eccentricity: | 0.0008010 |
| inclination: | 98.1281° |
| perigee height: | 625 km |
| apogee height: | 636 km |
| right ascension of ascending node: | 162.5269° |
| argument of perigee: | 186.8038° |
| revolutions per day: | 14.79484560 |
| mean anomaly at epoch: | 173.3066° |
| orbit number at epoch: | 84152 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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