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 4139U 69091B 24259.19667868 .00003009 00000-0 56699-3 0 9995
2 4139 74.0307 66.3901 0005964 209.3875 150.6958 14.64997931916343
Epoch (UTC): | 15 September 2024 04:43:13 |
Eccentricity: | 0.0005964 |
inclination: | 74.0307° |
perigee height: | 673 km |
apogee height: | 681 km |
right ascension of ascending node: | 66.3901° |
argument of perigee: | 209.3875° |
revolutions per day: | 14.64997931 |
mean anomaly at epoch: | 150.6958° |
orbit number at epoch: | 91634 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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