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 23271.98808695 .00000583 00000-0 21656-3 0 9991
2 39090 98.3863 102.5026 0008209 321.4339 38.6260 14.35702235554630
| Epoch (UTC): | 28 September 2023 23:42:50 |
| Eccentricity: | 0.0008209 |
| inclination: | 98.3863° |
| perigee height: | 767 km |
| apogee height: | 778 km |
| right ascension of ascending node: | 102.5026° |
| argument of perigee: | 321.4339° |
| revolutions per day: | 14.35702235 |
| mean anomaly at epoch: | 38.6260° |
| orbit number at epoch: | 55463 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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