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 33493U 09002B 23087.97117325 .00017287 00000-0 12327-2 0 9990
2 33493 98.2512 96.9660 0015410 319.3708 40.6365 15.04543241771681
Epoch (UTC): | 28 March 2023 23:18:29 |
Eccentricity: | 0.0015410 |
inclination: | 98.2512° |
perigee height: | 542 km |
apogee height: | 563 km |
right ascension of ascending node: | 96.9660° |
argument of perigee: | 319.3708° |
revolutions per day: | 15.04543241 |
mean anomaly at epoch: | 40.6365° |
orbit number at epoch: | 77168 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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