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 34574U 93036VL 23335.21274618 .00009445 00000-0 20370-2 0 9997
2 34574 74.0761 24.5100 0089845 245.6023 171.0972 14.55982565779244
Epoch (UTC): | 01 December 2023 05:06:21 |
Eccentricity: | 0.0089845 |
inclination: | 74.0761° |
perigee height: | 642 km |
apogee height: | 770 km |
right ascension of ascending node: | 24.5100° |
argument of perigee: | 245.6023° |
revolutions per day: | 14.55982565 |
mean anomaly at epoch: | 171.0972° |
orbit number at epoch: | 77924 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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