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 37481U 11019A 23088.85148889 -.00000010 00000-0 00000+0 0 9998
2 37481 2.2360 37.1017 0001846 331.6859 190.4220 1.00272331 43555
Epoch (UTC): | 29 March 2023 20:26:08 |
Eccentricity: | 0.0001846 |
inclination: | 2.2360° |
perigee height: | 35778 km |
apogee height: | 35794 km |
right ascension of ascending node: | 37.1017° |
argument of perigee: | 331.6859° |
revolutions per day: | 1.00272331 |
mean anomaly at epoch: | 190.4220° |
orbit number at epoch: | 4355 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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