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 34271U 93036LR 23335.89665899 .00012928 00000-0 34694-2 0 9994
2 34271 74.0289 173.1086 0032153 49.4052 14.3623 14.47860871774174
Epoch (UTC): | 01 December 2023 21:31:11 |
Eccentricity: | 0.0032153 |
inclination: | 74.0289° |
perigee height: | 710 km |
apogee height: | 755 km |
right ascension of ascending node: | 173.1086° |
argument of perigee: | 49.4052° |
revolutions per day: | 14.47860871 |
mean anomaly at epoch: | 14.3623° |
orbit number at epoch: | 77417 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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