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 11327U 79030B 22145.19061019 .00000062 00000-0 47188-4 0 9994
2 11327 82.9527 37.1717 0027790 169.7178 301.4307 13.76969810167269
| Epoch (UTC): | 25 May 2022 04:34:28 |
| Eccentricity: | 0.0027790 |
| inclination: | 82.9527° |
| perigee height: | 954 km |
| apogee height: | 995 km |
| right ascension of ascending node: | 37.1717° |
| argument of perigee: | 169.7178° |
| revolutions per day: | 13.76969810 |
| mean anomaly at epoch: | 301.4307° |
| orbit number at epoch: | 16726 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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