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 13552U 82092A 24301.23445417 .15659680 -12246-5 27896-3 0 9993
2 13552 82.5280 99.1133 0006890 255.2900 160.8321 16.47511674309572
| Epoch (UTC): | 27 October 2024 05:37:36 |
| Eccentricity: | 0.0006890 |
| inclination: | 82.5280° |
| perigee height: | 141 km |
| apogee height: | 150 km |
| right ascension of ascending node: | 99.1133° |
| argument of perigee: | 255.2900° |
| revolutions per day: | 16.47511674 |
| mean anomaly at epoch: | 160.8321° |
| orbit number at epoch: | 30957 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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