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 56527U 23065AA 24285.84065644 .00009024 00000-0 68184-3 0 9994
2 56527 43.0023 122.0083 0001354 275.8168 84.2520 15.02557428 78550
| Epoch (UTC): | 11 October 2024 20:10:32 |
| Eccentricity: | 0.0001354 |
| inclination: | 43.0023° |
| perigee height: | 558 km |
| apogee height: | 560 km |
| right ascension of ascending node: | 122.0083° |
| argument of perigee: | 275.8168° |
| revolutions per day: | 15.02557428 |
| mean anomaly at epoch: | 84.2520° |
| orbit number at epoch: | 7855 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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