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 32785U 08021C 22137.19331609 .00003280 00000-0 34986-3 0 9999
2 32785 97.6554 109.0392 0012198 345.5744 14.5124 14.89462311761909
| Epoch (UTC): | 17 May 2022 04:38:22 |
| Eccentricity: | 0.0012198 |
| inclination: | 97.6554° |
| perigee height: | 591 km |
| apogee height: | 608 km |
| right ascension of ascending node: | 109.0392° |
| argument of perigee: | 345.5744° |
| revolutions per day: | 14.89462311 |
| mean anomaly at epoch: | 14.5124° |
| orbit number at epoch: | 76190 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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