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 41465U 16026B 23090.85909813 .00038054 00000-0 59139-3 0 9992
2 41465 97.0109 323.6865 0008486 149.3669 271.1836 15.53811760387941
Epoch (UTC): | 31 March 2023 20:37:06 |
Eccentricity: | 0.0008486 |
inclination: | 97.0109° |
perigee height: | 400 km |
apogee height: | 411 km |
right ascension of ascending node: | 323.6865° |
argument of perigee: | 149.3669° |
revolutions per day: | 15.53811760 |
mean anomaly at epoch: | 271.1836° |
orbit number at epoch: | 38794 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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