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 33499U 09002H 23091.84104692 .00002560 00000-0 37216-3 0 9993
2 33499 98.1828 343.1573 0010121 108.8564 251.3744 14.76815515762799
Epoch (UTC): | 01 April 2023 20:11:06 |
Eccentricity: | 0.0010121 |
inclination: | 98.1828° |
perigee height: | 632 km |
apogee height: | 646 km |
right ascension of ascending node: | 343.1573° |
argument of perigee: | 108.8564° |
revolutions per day: | 14.76815515 |
mean anomaly at epoch: | 251.3744° |
orbit number at epoch: | 76279 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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