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 23334.69233813 .00021884 00000-0 46406-2 0 9999
2 34736 74.0319 72.9634 0016877 320.1517 154.7973 14.59018640774516
Epoch (UTC): | 30 November 2023 16:36:58 |
Eccentricity: | 0.0016877 |
inclination: | 74.0319° |
perigee height: | 684 km |
apogee height: | 708 km |
right ascension of ascending node: | 72.9634° |
argument of perigee: | 320.1517° |
revolutions per day: | 14.59018640 |
mean anomaly at epoch: | 154.7973° |
orbit number at epoch: | 77451 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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