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 40296U 14069A 23089.22696303 -.00000112 00000-0 00000+0 0 9998
2 40296 63.6009 352.3025 7144714 273.7886 345.8343 2.00633792 61656
Epoch (UTC): | 30 March 2023 05:26:49 |
Eccentricity: | 0.7144714 |
inclination: | 63.6009° |
perigee height: | 1204 km |
apogee height: | 39148 km |
right ascension of ascending node: | 352.3025° |
argument of perigee: | 273.7886° |
revolutions per day: | 2.00633792 |
mean anomaly at epoch: | 345.8343° |
orbit number at epoch: | 6165 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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