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 33591U 09005A 24281.17568037 .00000870 00000-0 48954-3 0 9997
2 33591 99.0345 338.0992 0013291 340.4108 19.6551 14.13144909807449
| Epoch (UTC): | 07 October 2024 04:12:58 |
| Eccentricity: | 0.0013291 |
| inclination: | 99.0345° |
| perigee height: | 839 km |
| apogee height: | 858 km |
| right ascension of ascending node: | 338.0992° |
| argument of perigee: | 340.4108° |
| revolutions per day: | 14.13144909 |
| mean anomaly at epoch: | 19.6551° |
| orbit number at epoch: | 80744 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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