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 14064U 83044A 23160.95322584 .00004001 00000-0 29135-3 0 9992
2 14064 65.0001 350.9950 0108364 260.8815 98.0031 15.00627472 49842
| Epoch (UTC): | 09 June 2023 22:52:38 |
| Eccentricity: | 0.0108364 |
| inclination: | 65.0001° |
| perigee height: | 490 km |
| apogee height: | 640 km |
| right ascension of ascending node: | 350.9950° |
| argument of perigee: | 260.8815° |
| revolutions per day: | 15.00627472 |
| mean anomaly at epoch: | 98.0031° |
| orbit number at epoch: | 4984 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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