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 38734U 12041B 24259.90515204 .00000072 00000-0 43979-3 0 9995
2 38734 82.4699 105.2157 0017100 23.3492 336.8362 12.44869416551128
Epoch (UTC): | 15 September 2024 21:43:25 |
Eccentricity: | 0.0017100 |
inclination: | 82.4699° |
perigee height: | 1472 km |
apogee height: | 1499 km |
right ascension of ascending node: | 105.2157° |
argument of perigee: | 23.3492° |
revolutions per day: | 12.44869416 |
mean anomaly at epoch: | 336.8362° |
orbit number at epoch: | 55112 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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