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 34736U 93036ZE 23333.45055747 .00018507 00000-0 39322-2 0 9997
2 34736 74.0321 75.3295 0016654 322.6269 112.6962 14.58965995774012
Epoch (UTC): | 29 November 2023 10:48:48 |
Eccentricity: | 0.0016654 |
inclination: | 74.0321° |
perigee height: | 685 km |
apogee height: | 708 km |
right ascension of ascending node: | 75.3295° |
argument of perigee: | 322.6269° |
revolutions per day: | 14.58965995 |
mean anomaly at epoch: | 112.6962° |
orbit number at epoch: | 77401 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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