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 39087U 13009B 23081.50394882 .00001456 00000-0 50911-3 0 9998
2 39087 98.3844 278.9032 0012711 153.5889 206.5949 14.36616873527494
| Epoch (UTC): | 22 March 2023 12:05:41 |
| Eccentricity: | 0.0012711 |
| inclination: | 98.3844° |
| perigee height: | 760 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 278.9032° |
| argument of perigee: | 153.5889° |
| revolutions per day: | 14.36616873 |
| mean anomaly at epoch: | 206.5949° |
| orbit number at epoch: | 52749 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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