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 00082U 61004B 24277.87633860 .00002326 00000-0 19706-2 0 9992
2 00082 38.8517 146.5175 1165374 99.5766 273.8263 12.27077918 445
| Epoch (UTC): | 03 October 2024 21:01:55 |
| Eccentricity: | 0.1165374 |
| inclination: | 38.8517° |
| perigee height: | 636 km |
| apogee height: | 2487 km |
| right ascension of ascending node: | 146.5175° |
| argument of perigee: | 99.5766° |
| revolutions per day: | 12.27077918 |
| mean anomaly at epoch: | 273.8263° |
| orbit number at epoch: | 44 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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