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 23081.20486556 -.00000140 00000-0 00000+0 0 9990
2 38093 3.2940 38.4444 0058540 357.5684 117.1945 1.00271869 40590
| Epoch (UTC): | 22 March 2023 04:55:00 |
| Eccentricity: | 0.0058540 |
| inclination: | 3.2940° |
| perigee height: | 35539 km |
| apogee height: | 36033 km |
| right ascension of ascending node: | 38.4444° |
| argument of perigee: | 357.5684° |
| revolutions per day: | 1.00271869 |
| mean anomaly at epoch: | 117.1945° |
| orbit number at epoch: | 4059 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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