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 12278U 78026DW 24276.83531010 .00020315 00000-0 65164-2 0 9990
2 12278 99.0968 53.5667 0042319 351.9606 164.9663 14.38952651253610
Epoch (UTC): | 02 October 2024 20:02:50 |
Eccentricity: | 0.0042319 |
inclination: | 99.0968° |
perigee height: | 732 km |
apogee height: | 792 km |
right ascension of ascending node: | 53.5667° |
argument of perigee: | 351.9606° |
revolutions per day: | 14.38952651 |
mean anomaly at epoch: | 164.9663° |
orbit number at epoch: | 25361 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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