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 33956U 97051BR 22291.06039237 .09164539 21371+0 34639-1 0 9990
2 33956 86.3499 128.8308 0008980 310.5420 49.5081 15.95684307477909
Epoch (UTC): | 18 October 2022 01:26:57 |
Eccentricity: | 0.0008980 |
inclination: | 86.3499° |
perigee height: | 280 km |
apogee height: | 292 km |
right ascension of ascending node: | 128.8308° |
argument of perigee: | 310.5420° |
revolutions per day: | 15.95684307 |
mean anomaly at epoch: | 49.5081° |
orbit number at epoch: | 47790 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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