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 27386U 02009A 24307.14047583 .00000867 00000-0 29619-3 0 9996
2 27386 98.3018 263.5652 0001346 84.5685 285.9637 14.38739134188411
Epoch (UTC): | 02 November 2024 03:22:17 |
Eccentricity: | 0.0001346 |
inclination: | 98.3018° |
perigee height: | 762 km |
apogee height: | 763 km |
right ascension of ascending node: | 263.5652° |
argument of perigee: | 84.5685° |
revolutions per day: | 14.38739134 |
mean anomaly at epoch: | 285.9637° |
orbit number at epoch: | 18841 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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