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 23151.88945864 .00002977 00000-0 22055-3 0 9990
2 14064 65.0003 19.3502 0108586 263.8735 95.0004 15.00558492 48484
| Epoch (UTC): | 31 May 2023 21:20:49 |
| Eccentricity: | 0.0108586 |
| inclination: | 65.0003° |
| perigee height: | 490 km |
| apogee height: | 640 km |
| right ascension of ascending node: | 19.3502° |
| argument of perigee: | 263.8735° |
| revolutions per day: | 15.00558492 |
| mean anomaly at epoch: | 95.0004° |
| orbit number at epoch: | 4848 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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