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 23266.59418730 -.00000128 00000-0 00000-0 0 9993
2 38093 3.5785 41.5472 0051685 2.9770 71.5911 1.00272522 42445
Epoch (UTC): | 23 September 2023 14:15:37 |
Eccentricity: | 0.0051685 |
inclination: | 3.5785° |
perigee height: | 35568 km |
apogee height: | 36004 km |
right ascension of ascending node: | 41.5472° |
argument of perigee: | 2.9770° |
revolutions per day: | 1.00272522 |
mean anomaly at epoch: | 71.5911° |
orbit number at epoch: | 4244 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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