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 19274U 88056A 22145.52816069 .00002695 00000-0 17471-3 0 9996
2 19274 82.5036 196.3045 0008139 283.5173 76.5148 15.07710947825228
| Epoch (UTC): | 25 May 2022 12:40:33 |
| Eccentricity: | 0.0008139 |
| inclination: | 82.5036° |
| perigee height: | 537 km |
| apogee height: | 549 km |
| right ascension of ascending node: | 196.3045° |
| argument of perigee: | 283.5173° |
| revolutions per day: | 15.07710947 |
| mean anomaly at epoch: | 76.5148° |
| orbit number at epoch: | 82522 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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