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 17590U 87027B 23028.58353668 .00000305 00000-0 17622-3 0 9994
2 17590 71.0033 149.9091 0003446 31.9987 328.1345 14.16854843854440
| Epoch (UTC): | 28 January 2023 14:00:17 |
| Eccentricity: | 0.0003446 |
| inclination: | 71.0033° |
| perigee height: | 833 km |
| apogee height: | 838 km |
| right ascension of ascending node: | 149.9091° |
| argument of perigee: | 31.9987° |
| revolutions per day: | 14.16854843 |
| mean anomaly at epoch: | 328.1345° |
| orbit number at epoch: | 85444 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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