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 23561U 95021B 24276.64129983 .00001787 00000-0 59228-3 0 9999
2 23561 98.5172 342.4107 0005686 266.2460 238.0820 14.39083252543993
| Epoch (UTC): | 02 October 2024 15:23:28 |
| Eccentricity: | 0.0005686 |
| inclination: | 98.5172° |
| perigee height: | 757 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 342.4107° |
| argument of perigee: | 266.2460° |
| revolutions per day: | 14.39083252 |
| mean anomaly at epoch: | 238.0820° |
| orbit number at epoch: | 54399 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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