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 19046U 88032B 24308.57851651 .00014728 00000-0 83528-3 0 9997
2 19046 97.4649 286.8762 0031778 135.6842 224.6942 15.12632167977663
Epoch (UTC): | 03 November 2024 13:53:03 |
Eccentricity: | 0.0031778 |
inclination: | 97.4649° |
perigee height: | 506 km |
apogee height: | 550 km |
right ascension of ascending node: | 286.8762° |
argument of perigee: | 135.6842° |
revolutions per day: | 15.12632167 |
mean anomaly at epoch: | 224.6942° |
orbit number at epoch: | 97766 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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