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 22144.81874953 .00000046 00000-0 31275-4 0 9993
2 11327 82.9527 37.4477 0027775 170.7307 258.1115 13.76969682166995
| Epoch (UTC): | 24 May 2022 19:38:59 |
| Eccentricity: | 0.0027775 |
| inclination: | 82.9527° |
| perigee height: | 954 km |
| apogee height: | 995 km |
| right ascension of ascending node: | 37.4477° |
| argument of perigee: | 170.7307° |
| revolutions per day: | 13.76969682 |
| mean anomaly at epoch: | 258.1115° |
| orbit number at epoch: | 16699 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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