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 14051U 83041B 24287.83729249 .00018174 00000-0 16579-2 0 9995
2 14051 25.3305 219.4190 1022984 342.6327 14.1505 13.25451045930299
Epoch (UTC): | 13 October 2024 20:05:42 |
Eccentricity: | 0.1022984 |
inclination: | 25.3305° |
perigee height: | 392 km |
apogee height: | 1935 km |
right ascension of ascending node: | 219.4190° |
argument of perigee: | 342.6327° |
revolutions per day: | 13.25451045 |
mean anomaly at epoch: | 14.1505° |
orbit number at epoch: | 93029 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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