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 37570U 10038F 22222.26001788 .00001030 00000-0 21988-3 0 9991
2 37570 97.9089 331.2384 0175847 350.0018 9.7696 14.51742411632546
| Epoch (UTC): | 10 August 2022 06:14:25 |
| Eccentricity: | 0.0175847 |
| inclination: | 97.9089° |
| perigee height: | 595 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 331.2384° |
| argument of perigee: | 350.0018° |
| revolutions per day: | 14.51742411 |
| mean anomaly at epoch: | 9.7696° |
| orbit number at epoch: | 63254 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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