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 23947U 96038C 25195.95193487 .00000506 00000-0 29755-3 0 9991
2 23947 55.3088 116.5157 4955668 80.6327 330.0744 5.56802073121787
Epoch (UTC): | 14 July 2025 22:50:47 |
Eccentricity: | 0.4955668 |
inclination: | 55.3088° |
perigee height: | 404 km |
apogee height: | 13731 km |
right ascension of ascending node: | 116.5157° |
argument of perigee: | 80.6327° |
revolutions per day: | 5.56802073 |
mean anomaly at epoch: | 330.0744° |
orbit number at epoch: | 12178 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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