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 55734U 14028AW 24277.68476373 .00111647 00000-0 12920+0 0 9998
2 55734 82.3518 265.7672 0187384 164.5431 196.1550 13.61097295 15896
Epoch (UTC): | 03 October 2024 16:26:03 |
Eccentricity: | 0.0187384 |
inclination: | 82.3518° |
perigee height: | 893 km |
apogee height: | 1170 km |
right ascension of ascending node: | 265.7672° |
argument of perigee: | 164.5431° |
revolutions per day: | 13.61097295 |
mean anomaly at epoch: | 196.1550° |
orbit number at epoch: | 1589 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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