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 15543U 85010B 22200.95036542 0.00000000 00000-0 00000-0 0 05
2 15543 15.1799 328.1529 0125174 17.9552 342.4949 0.99809947 01
| Epoch (UTC): | 19 July 2022 22:48:31 |
| Eccentricity: | 0.0125174 |
| inclination: | 15.1799° |
| perigee height: | 35387 km |
| apogee height: | 36445 km |
| right ascension of ascending node: | 328.1529° |
| argument of perigee: | 17.9552° |
| revolutions per day: | 0.99809947 |
| mean anomaly at epoch: | 342.4949° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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