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 6324U 72104B 24310.72817951 .00001242 00000-0 36556-3 0 9996
2 6324 74.0754 142.8195 0009467 302.5846 57.4397 14.44688283724992
Epoch (UTC): | 05 November 2024 17:28:34 |
Eccentricity: | 0.0009467 |
inclination: | 74.0754° |
perigee height: | 736 km |
apogee height: | 750 km |
right ascension of ascending node: | 142.8195° |
argument of perigee: | 302.5846° |
revolutions per day: | 14.44688283 |
mean anomaly at epoch: | 57.4397° |
orbit number at epoch: | 72499 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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