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 39232U 13043A 23263.85431359 0.00047000 00000-0 45185-3 0 04
2 39232 97.8641 325.1490 0521862 120.5277 239.4721 14.80238971 09
Epoch (UTC): | 20 September 2023 20:30:12 |
Eccentricity: | 0.0521862 |
inclination: | 97.8641° |
perigee height: | 263 km |
apogee height: | 994 km |
right ascension of ascending node: | 325.1490° |
argument of perigee: | 120.5277° |
revolutions per day: | 14.80238971 |
mean anomaly at epoch: | 239.4721° |
orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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