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 23334.50026827 .00000904 00000-0 32703-3 0 9990
2 39090 98.3805 163.2928 0009758 124.3954 235.8156 14.35795500563603
| Epoch (UTC): | 30 November 2023 12:00:23 |
| Eccentricity: | 0.0009758 |
| inclination: | 98.3805° |
| perigee height: | 765 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 163.2928° |
| argument of perigee: | 124.3954° |
| revolutions per day: | 14.35795500 |
| mean anomaly at epoch: | 235.8156° |
| orbit number at epoch: | 56360 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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