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 39664U 87060AB 24357.36940641 .00000861 00000-0 34885-3 0 9999
2 39664 65.0064 93.4010 0019889 262.1853 97.6975 14.33160187558892
| Epoch (UTC): | 22 December 2024 08:51:56 |
| Eccentricity: | 0.0019889 |
| inclination: | 65.0064° |
| perigee height: | 767 km |
| apogee height: | 795 km |
| right ascension of ascending node: | 93.4010° |
| argument of perigee: | 262.1853° |
| revolutions per day: | 14.33160187 |
| mean anomaly at epoch: | 97.6975° |
| orbit number at epoch: | 55889 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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