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 39089U 13009D 24357.54540674 .00000429 00000-0 16396-3 0 9991
2 39089 98.4006 180.0131 0012079 63.6759 296.5666 14.35439391619027
| Epoch (UTC): | 22 December 2024 13:05:23 |
| Eccentricity: | 0.0012079 |
| inclination: | 98.4006° |
| perigee height: | 765 km |
| apogee height: | 782 km |
| right ascension of ascending node: | 180.0131° |
| argument of perigee: | 63.6759° |
| revolutions per day: | 14.35439391 |
| mean anomaly at epoch: | 296.5666° |
| orbit number at epoch: | 61902 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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