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 38093U 12009A 23341.53576009 -.00000102 00000-0 00000-0 0 9997
2 38093 3.7053 42.6210 0050920 357.1960 129.1446 1.00270699 43193
Epoch (UTC): | 07 December 2023 12:51:29 |
Eccentricity: | 0.0050920 |
inclination: | 3.7053° |
perigee height: | 35572 km |
apogee height: | 36001 km |
right ascension of ascending node: | 42.6210° |
argument of perigee: | 357.1960° |
revolutions per day: | 1.00270699 |
mean anomaly at epoch: | 129.1446° |
orbit number at epoch: | 4319 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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