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 20580U 90037B 23334.05431826 .00008754 00000-0 44591-3 0 9998
2 20580 28.4682 243.0350 0002681 18.2914 108.2920 15.15040290646887
| Epoch (UTC): | 30 November 2023 01:18:13 |
| Eccentricity: | 0.0002681 |
| inclination: | 28.4682° |
| perigee height: | 519 km |
| apogee height: | 523 km |
| right ascension of ascending node: | 243.0350° |
| argument of perigee: | 18.2914° |
| revolutions per day: | 15.15040290 |
| mean anomaly at epoch: | 108.2920° |
| orbit number at epoch: | 64688 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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