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 00029U 60002B 24317.92382904 .00002526 00000-0 38068-3 0 9996
2 00029 48.3778 264.2800 0023028 286.3800 73.4582 14.77218983456143
Epoch (UTC): | 12 November 2024 22:10:18 |
Eccentricity: | 0.0023028 |
inclination: | 48.3778° |
perigee height: | 622 km |
apogee height: | 654 km |
right ascension of ascending node: | 264.2800° |
argument of perigee: | 286.3800° |
revolutions per day: | 14.77218983 |
mean anomaly at epoch: | 73.4582° |
orbit number at epoch: | 45614 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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