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 39090U 13009E 23339.51779620 .00000537 00000-0 20029-3 0 9992
2 39090 98.3801 168.1711 0009906 110.7466 249.4783 14.35802046564304
| Epoch (UTC): | 05 December 2023 12:25:37 |
| Eccentricity: | 0.0009906 |
| inclination: | 98.3801° |
| perigee height: | 765 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 168.1711° |
| argument of perigee: | 110.7466° |
| revolutions per day: | 14.35802046 |
| mean anomaly at epoch: | 249.4783° |
| orbit number at epoch: | 56430 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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