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 00029U 60002B 24311.90377755 .00003907 00000-0 57303-3 0 9993
2 00029 48.3779 292.8192 0023115 261.3287 98.5007 14.77175404455255
Epoch (UTC): | 06 November 2024 21:41:26 |
Eccentricity: | 0.0023115 |
inclination: | 48.3779° |
perigee height: | 622 km |
apogee height: | 654 km |
right ascension of ascending node: | 292.8192° |
argument of perigee: | 261.3287° |
revolutions per day: | 14.77175404 |
mean anomaly at epoch: | 98.5007° |
orbit number at epoch: | 45525 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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