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 29164U 06020C 23266.69288976 .00106845 00000-0 55897-2 0 9994
2 29164 6.8169 20.6788 3953810 37.2539 344.5665 7.53713157311178
Epoch (UTC): | 23 September 2023 16:37:45 |
Eccentricity: | 0.3953810 |
inclination: | 6.8169° |
perigee height: | 265 km |
apogee height: | 8954 km |
right ascension of ascending node: | 20.6788° |
argument of perigee: | 37.2539° |
revolutions per day: | 7.53713157 |
mean anomaly at epoch: | 344.5665° |
orbit number at epoch: | 31117 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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