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 60774U 24140EZ 24356.97598549 .00037223 00000-0 54708-2 0 9994
2 60774 89.3533 340.8425 0139453 253.3419 105.2450 14.68837902 19268
| Epoch (UTC): | 21 December 2024 23:25:25 |
| Eccentricity: | 0.0139453 |
| inclination: | 89.3533° |
| perigee height: | 566 km |
| apogee height: | 763 km |
| right ascension of ascending node: | 340.8425° |
| argument of perigee: | 253.3419° |
| revolutions per day: | 14.68837902 |
| mean anomaly at epoch: | 105.2450° |
| orbit number at epoch: | 1926 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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