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 is defined by the following mean orbital elements,
1 23560U 95021A 24052.65943318 .32169375 33451-5 24835-3 0 9997
2 23560 98.4779 71.8096 0011047 264.7570 236.2294 16.52434583548081
| Epoch (UTC): | 21 February 2024 15:49:35 |
| Eccentricity: | 0.0011047 |
| inclination: | 98.4779° |
| perigee height: | 126 km |
| apogee height: | 140 km |
| right ascension of ascending node: | 71.8096° |
| argument of perigee: | 264.7570° |
| revolutions per day: | 16.52434583 |
| mean anomaly at epoch: | 236.2294° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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