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 43005U 17070A 24358.15610070 .00001910 00000-0 27786-3 0 9993
2 43005 97.9571 67.2384 0001399 82.8265 277.3104 14.77055596384115
| Epoch (UTC): | 23 December 2024 03:44:47 |
| Eccentricity: | 0.0001399 |
| inclination: | 97.9571° |
| perigee height: | 637 km |
| apogee height: | 639 km |
| right ascension of ascending node: | 67.2384° |
| argument of perigee: | 82.8265° |
| revolutions per day: | 14.77055596 |
| mean anomaly at epoch: | 277.3104° |
| orbit number at epoch: | 38411 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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