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 42017U 17008BX 23081.77861001 .00099059 00000-0 14544-2 0 9996
2 42017 97.2239 150.8817 0002112 296.2456 63.8582 15.55163467339941
Epoch (UTC): | 22 March 2023 18:41:11 |
Eccentricity: | 0.0002112 |
inclination: | 97.2239° |
perigee height: | 400 km |
apogee height: | 403 km |
right ascension of ascending node: | 150.8817° |
argument of perigee: | 296.2456° |
revolutions per day: | 15.55163467 |
mean anomaly at epoch: | 63.8582° |
orbit number at epoch: | 33994 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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