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 24261.74944170 .00027155 00000-0 30214-2 0 9991
2 33498 98.1137 177.8642 0011894 102.7595 257.4950 14.87037463843421
| Epoch (UTC): | 17 September 2024 17:59:11 |
| Eccentricity: | 0.0011894 |
| inclination: | 98.1137° |
| perigee height: | 599 km |
| apogee height: | 615 km |
| right ascension of ascending node: | 177.8642° |
| argument of perigee: | 102.7595° |
| revolutions per day: | 14.87037463 |
| mean anomaly at epoch: | 257.4950° |
| orbit number at epoch: | 84342 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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