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 35946U 09055A 24358.18378593 .00000384 00000-0 14395-3 0 9992
2 35946 98.4915 68.2291 0004748 44.0318 316.1246 14.37049706798037
| Epoch (UTC): | 23 December 2024 04:24:39 |
| Eccentricity: | 0.0004748 |
| inclination: | 98.4915° |
| perigee height: | 765 km |
| apogee height: | 771 km |
| right ascension of ascending node: | 68.2291° |
| argument of perigee: | 44.0318° |
| revolutions per day: | 14.37049706 |
| mean anomaly at epoch: | 316.1246° |
| orbit number at epoch: | 79803 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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