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 23031.45944840 .00007510 00000-0 56438-3 0 9993
2 14064 65.0011 35.5883 0108367 304.3287 54.7612 14.98642338 30381
| Epoch (UTC): | 31 January 2023 11:01:36 |
| Eccentricity: | 0.0108367 |
| inclination: | 65.0011° |
| perigee height: | 496 km |
| apogee height: | 646 km |
| right ascension of ascending node: | 35.5883° |
| argument of perigee: | 304.3287° |
| revolutions per day: | 14.98642338 |
| mean anomaly at epoch: | 54.7612° |
| orbit number at epoch: | 3038 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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