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 39483U 13076A 23084.10700044 .00000010 00000-0 -20353-5 0 9997
2 39483 82.4891 184.1060 0020349 145.5849 214.6557 12.42894585419490
| Epoch (UTC): | 25 March 2023 02:34:04 |
| Eccentricity: | 0.0020349 |
| inclination: | 82.4891° |
| perigee height: | 1478 km |
| apogee height: | 1510 km |
| right ascension of ascending node: | 184.1060° |
| argument of perigee: | 145.5849° |
| revolutions per day: | 12.42894585 |
| mean anomaly at epoch: | 214.6557° |
| orbit number at epoch: | 41949 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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