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 25774U 99031E 23147.73666501 -.00000100 00000-0 37616-4 0 9997
2 25774 51.5279 304.3876 0374720 26.2972 347.5450 13.46540570178883
| Epoch (UTC): | 27 May 2023 17:40:47 |
| Eccentricity: | 0.0374720 |
| inclination: | 51.5279° |
| perigee height: | 805 km |
| apogee height: | 1364 km |
| right ascension of ascending node: | 304.3876° |
| argument of perigee: | 26.2972° |
| revolutions per day: | 13.46540570 |
| mean anomaly at epoch: | 347.5450° |
| orbit number at epoch: | 17888 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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