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 21017.48612825 -.00000120 00000-0 13233-4 0 9996
2 00029 48.3807 18.5032 0023425 67.5506 292.7884 14.74398393250128
Epoch (UTC): | 17 January 2021 11:40:01 |
Eccentricity: | 0.0023425 |
inclination: | 48.3807° |
perigee height: | 630 km |
apogee height: | 663 km |
right ascension of ascending node: | 18.5032° |
argument of perigee: | 67.5506° |
revolutions per day: | 14.74398393 |
mean anomaly at epoch: | 292.7884° |
orbit number at epoch: | 25012 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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