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 24255.61394587 .00002766 00000-0 10318-2 0 9999
2 39658 65.0134 15.3832 0020813 262.2958 97.5764 14.33516591544494
| Epoch (UTC): | 11 September 2024 14:44:04 |
| Eccentricity: | 0.0020813 |
| inclination: | 65.0134° |
| perigee height: | 765 km |
| apogee height: | 795 km |
| right ascension of ascending node: | 15.3832° |
| argument of perigee: | 262.2958° |
| revolutions per day: | 14.33516591 |
| mean anomaly at epoch: | 97.5764° |
| orbit number at epoch: | 54449 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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