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 39658U 87060V 23331.78968692 .00001200 00000-0 47449-3 0 9993
2 39658 65.0101 106.4062 0018965 280.9993 78.8959 14.32865004503102
| Epoch (UTC): | 27 November 2023 18:57:08 |
| Eccentricity: | 0.0018965 |
| inclination: | 65.0101° |
| perigee height: | 768 km |
| apogee height: | 796 km |
| right ascension of ascending node: | 106.4062° |
| argument of perigee: | 280.9993° |
| revolutions per day: | 14.32865004 |
| mean anomaly at epoch: | 78.8959° |
| orbit number at epoch: | 50310 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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