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 15483U 85006B 24282.34878485 .00002529 00000-0 85563-3 0 9993
2 15483 74.0443 132.7425 0018729 178.5131 354.3430 14.37246029 79952
| Epoch (UTC): | 08 October 2024 08:22:15 |
| Eccentricity: | 0.0018729 |
| inclination: | 74.0443° |
| perigee height: | 754 km |
| apogee height: | 781 km |
| right ascension of ascending node: | 132.7425° |
| argument of perigee: | 178.5131° |
| revolutions per day: | 14.37246029 |
| mean anomaly at epoch: | 354.3430° |
| orbit number at epoch: | 7995 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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