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 24357.45847294 .00017875 00000-0 88566-3 0 9992
2 14064 64.9948 17.5480 0059923 16.9340 343.3767 15.16277546134402
| Epoch (UTC): | 22 December 2024 11:00:12 |
| Eccentricity: | 0.0059923 |
| inclination: | 64.9948° |
| perigee height: | 476 km |
| apogee height: | 558 km |
| right ascension of ascending node: | 17.5480° |
| argument of perigee: | 16.9340° |
| revolutions per day: | 15.16277546 |
| mean anomaly at epoch: | 343.3767° |
| orbit number at epoch: | 13440 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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