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 6155U 72065B 24276.91401874 .00008096 00000-0 11685-2 0 9998
2 6155 35.0010 124.5410 0036153 296.5868 63.1129 14.75178983784854
| Epoch (UTC): | 02 October 2024 21:56:11 |
| Eccentricity: | 0.0036153 |
| inclination: | 35.0010° |
| perigee height: | 619 km |
| apogee height: | 670 km |
| right ascension of ascending node: | 124.5410° |
| argument of perigee: | 296.5868° |
| revolutions per day: | 14.75178983 |
| mean anomaly at epoch: | 63.1129° |
| orbit number at epoch: | 78485 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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