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 53754U 22107BG 24279.81944692 .00021674 00000-0 11842-2 0 9991
2 53754 53.2382 304.6781 0434117 305.6769 50.4514 14.58937706111747
Epoch (UTC): | 05 October 2024 19:40:00 |
Eccentricity: | 0.0434117 |
inclination: | 53.2382° |
perigee height: | 389 km |
apogee height: | 1004 km |
right ascension of ascending node: | 304.6781° |
argument of perigee: | 305.6769° |
revolutions per day: | 14.58937706 |
mean anomaly at epoch: | 50.4514° |
orbit number at epoch: | 11174 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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