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 29973U 99025KX 24358.48364965 .00002712 00000-0 16724-2 0 9996
2 29973 98.8378 1.4012 0060773 63.2048 96.5029 14.05335175917506
Epoch (UTC): | 23 December 2024 11:36:27 |
Eccentricity: | 0.0060773 |
inclination: | 98.8378° |
perigee height: | 831 km |
apogee height: | 919 km |
right ascension of ascending node: | 1.4012° |
argument of perigee: | 63.2048° |
revolutions per day: | 14.05335175 |
mean anomaly at epoch: | 96.5029° |
orbit number at epoch: | 91750 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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