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 25544U 98067A 24349.89091016 .00016122 00000-0 28371-3 0 9992
2 25544 51.6383 140.0943 0007387 343.4355 180.2578 15.50592659486579
| Epoch (UTC): | 14 December 2024 21:22:54 |
| Eccentricity: | 0.0007387 |
| inclination: | 51.6383° |
| perigee height: | 410 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 140.0943° |
| argument of perigee: | 343.4355° |
| revolutions per day: | 15.50592659 |
| mean anomaly at epoch: | 180.2578° |
| orbit number at epoch: | 48657 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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