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 23147.42408026 .00002415 00000-0 18162-3 0 9990
2 14064 65.0003 33.3176 0108613 265.3602 93.5106 15.00530414 47814
| Epoch (UTC): | 27 May 2023 10:10:40 |
| Eccentricity: | 0.0108613 |
| inclination: | 65.0003° |
| perigee height: | 490 km |
| apogee height: | 640 km |
| right ascension of ascending node: | 33.3176° |
| argument of perigee: | 265.3602° |
| revolutions per day: | 15.00530414 |
| mean anomaly at epoch: | 93.5106° |
| orbit number at epoch: | 4781 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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