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 23026.98319967 .00000336 00000-0 32749-3 0 9996
2 00082 38.8530 267.9209 1167505 5.1701 355.9930 12.26085517924841
| Epoch (UTC): | 26 January 2023 23:35:48 |
| Eccentricity: | 0.1167505 |
| inclination: | 38.8530° |
| perigee height: | 638 km |
| apogee height: | 2493 km |
| right ascension of ascending node: | 267.9209° |
| argument of perigee: | 5.1701° |
| revolutions per day: | 12.26085517 |
| mean anomaly at epoch: | 355.9930° |
| orbit number at epoch: | 92484 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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