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 39446U 13066AG 23276.42601547 .00007633 00000-0 91313-3 0 9990
2 39446 97.7465 227.8468 0064035 346.7374 13.2154 14.82950786531055
Epoch (UTC): | 03 October 2023 10:13:27 |
Eccentricity: | 0.0064035 |
inclination: | 97.7465° |
perigee height: | 575 km |
apogee height: | 665 km |
right ascension of ascending node: | 227.8468° |
argument of perigee: | 346.7374° |
revolutions per day: | 14.82950786 |
mean anomaly at epoch: | 13.2154° |
orbit number at epoch: | 53105 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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