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 11427U 79060B 24277.17587691 .00001496 00000-0 49923-3 0 9993
2 11427 74.0166 156.7352 0019213 15.4799 344.6938 14.38301919370872
| Epoch (UTC): | 03 October 2024 04:13:15 |
| Eccentricity: | 0.0019213 |
| inclination: | 74.0166° |
| perigee height: | 750 km |
| apogee height: | 778 km |
| right ascension of ascending node: | 156.7352° |
| argument of perigee: | 15.4799° |
| revolutions per day: | 14.38301919 |
| mean anomaly at epoch: | 344.6938° |
| orbit number at epoch: | 37087 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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