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 40056U 14034D 23080.46464515 .00002326 00000-0 34384-3 0 9993
2 40056 98.3830 252.0709 0013789 192.9345 167.1511 14.76196253460381
Epoch (UTC): | 21 March 2023 11:09:05 |
Eccentricity: | 0.0013789 |
inclination: | 98.3830° |
perigee height: | 631 km |
apogee height: | 651 km |
right ascension of ascending node: | 252.0709° |
argument of perigee: | 192.9345° |
revolutions per day: | 14.76196253 |
mean anomaly at epoch: | 167.1511° |
orbit number at epoch: | 46038 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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