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 22176.48392812 .00002897 00000-0 23857-3 0 9992
2 33493 98.2252 163.5126 0015947 142.6615 217.5718 14.99867104730186
Epoch (UTC): | 25 June 2022 11:36:51 |
Eccentricity: | 0.0015947 |
inclination: | 98.2252° |
perigee height: | 556 km |
apogee height: | 578 km |
right ascension of ascending node: | 163.5126° |
argument of perigee: | 142.6615° |
revolutions per day: | 14.99867104 |
mean anomaly at epoch: | 217.5718° |
orbit number at epoch: | 73018 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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