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 38342U 12026A 23267.90952170 -.00000182 00000-0 00000-0 0 9996
2 38342 0.0203 160.6722 0002850 26.5822 52.5450 1.00269898 40436
| Epoch (UTC): | 24 September 2023 21:49:42 |
| Eccentricity: | 0.0002850 |
| inclination: | 0.0203° |
| perigee height: | 35775 km |
| apogee height: | 35799 km |
| right ascension of ascending node: | 160.6722° |
| argument of perigee: | 26.5822° |
| revolutions per day: | 1.00269898 |
| mean anomaly at epoch: | 52.5450° |
| orbit number at epoch: | 4043 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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