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 00876U 64053A 23151.98114684 .00000116 00000-0 41967-4 0 9991
2 00876 65.0612 8.4712 0145203 332.3578 26.9855 14.64215477125746
| Epoch (UTC): | 31 May 2023 23:32:51 |
| Eccentricity: | 0.0145203 |
| inclination: | 65.0612° |
| perigee height: | 577 km |
| apogee height: | 782 km |
| right ascension of ascending node: | 8.4712° |
| argument of perigee: | 332.3578° |
| revolutions per day: | 14.64215477 |
| mean anomaly at epoch: | 26.9855° |
| orbit number at epoch: | 12574 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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