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 23152.88915829 .00003400 00000-0 24995-3 0 9996
2 14064 65.0002 16.2229 0108555 263.5448 95.3301 15.00566381 48590
| Epoch (UTC): | 01 June 2023 21:20:23 |
| Eccentricity: | 0.0108555 |
| inclination: | 65.0002° |
| perigee height: | 490 km |
| apogee height: | 640 km |
| right ascension of ascending node: | 16.2229° |
| argument of perigee: | 263.5448° |
| revolutions per day: | 15.00566381 |
| mean anomaly at epoch: | 95.3301° |
| orbit number at epoch: | 4859 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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