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 22176.21707327 .00003154 00000-0 25928-3 0 9992
2 33493 98.2253 163.2306 0015919 143.4547 216.7764 14.99865940730151
Epoch (UTC): | 25 June 2022 05:12:35 |
Eccentricity: | 0.0015919 |
inclination: | 98.2253° |
perigee height: | 556 km |
apogee height: | 578 km |
right ascension of ascending node: | 163.2306° |
argument of perigee: | 143.4547° |
revolutions per day: | 14.99865940 |
mean anomaly at epoch: | 216.7764° |
orbit number at epoch: | 73015 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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