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 24260.93443711 .00000022 00000-0 89435-4 0 9997
2 39483 82.4862 206.4268 0020593 47.1307 313.1498 12.42891184486601
| Epoch (UTC): | 16 September 2024 22:25:35 |
| Eccentricity: | 0.0020593 |
| inclination: | 82.4862° |
| perigee height: | 1478 km |
| apogee height: | 1510 km |
| right ascension of ascending node: | 206.4268° |
| argument of perigee: | 47.1307° |
| revolutions per day: | 12.42891184 |
| mean anomaly at epoch: | 313.1498° |
| orbit number at epoch: | 48660 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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