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 35571U 08053G 24278.08924646 .00034977 00000-0 45706-2 0 9993
2 35571 97.6768 320.4370 0131724 308.7154 50.2336 14.74408280840437
| Epoch (UTC): | 04 October 2024 02:08:30 |
| Eccentricity: | 0.0131724 |
| inclination: | 97.6768° |
| perigee height: | 554 km |
| apogee height: | 739 km |
| right ascension of ascending node: | 320.4370° |
| argument of perigee: | 308.7154° |
| revolutions per day: | 14.74408280 |
| mean anomaly at epoch: | 50.2336° |
| orbit number at epoch: | 84043 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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