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 3741U 63047L 24253.18916098 .00030844 00000-0 71423-2 0 9991
2 3741 29.8777 199.7894 0279046 71.2539 291.8122 14.32912169819651
Epoch (UTC): | 09 September 2024 04:32:23 |
Eccentricity: | 0.0279046 |
inclination: | 29.8777° |
perigee height: | 582 km |
apogee height: | 982 km |
right ascension of ascending node: | 199.7894° |
argument of perigee: | 71.2539° |
revolutions per day: | 14.32912169 |
mean anomaly at epoch: | 291.8122° |
orbit number at epoch: | 81965 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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