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 23335.47590118 .00000852 00000-0 30906-3 0 9991
2 39090 98.3804 164.2414 0009793 121.7843 238.4298 14.35796882563723
| Epoch (UTC): | 01 December 2023 11:25:17 |
| Eccentricity: | 0.0009793 |
| inclination: | 98.3804° |
| perigee height: | 765 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 164.2414° |
| argument of perigee: | 121.7843° |
| revolutions per day: | 14.35796882 |
| mean anomaly at epoch: | 238.4298° |
| orbit number at epoch: | 56372 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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