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 14033U 83037B 23156.39289951 .00000511 00000-0 57773-4 0 9995
2 14033 82.5067 100.7870 0018893 123.1400 237.1631 14.84375665781675
Epoch (UTC): | 05 June 2023 09:25:46 |
Eccentricity: | 0.0018893 |
inclination: | 82.5067° |
perigee height: | 602 km |
apogee height: | 629 km |
right ascension of ascending node: | 100.7870° |
argument of perigee: | 123.1400° |
revolutions per day: | 14.84375665 |
mean anomaly at epoch: | 237.1631° |
orbit number at epoch: | 78167 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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