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 43479U 18047D 24357.97720224 .00000099 00000-0 28237-4 0 9995
2 43479 86.3961 314.4959 0002186 83.5871 276.5574 14.34217560344927
| Epoch (UTC): | 22 December 2024 23:27:10 |
| Eccentricity: | 0.0002186 |
| inclination: | 86.3961° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 314.4959° |
| argument of perigee: | 83.5871° |
| revolutions per day: | 14.34217560 |
| mean anomaly at epoch: | 276.5574° |
| orbit number at epoch: | 34492 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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