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 25634U 99008A 24280.70339514 .00000585 00000-0 29581-3 0 9990
2 25634 98.4318 262.1552 0010944 39.2095 320.9873 14.19744645326530
| Epoch (UTC): | 06 October 2024 16:52:53 |
| Eccentricity: | 0.0010944 |
| inclination: | 98.4318° |
| perigee height: | 818 km |
| apogee height: | 834 km |
| right ascension of ascending node: | 262.1552° |
| argument of perigee: | 39.2095° |
| revolutions per day: | 14.19744645 |
| mean anomaly at epoch: | 320.9873° |
| orbit number at epoch: | 32653 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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