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 39430U 13066Q 22273.97664690 .00001339 00000-0 24469-3 0 9992
2 39430 97.7988 175.1103 0150279 72.2544 289.5012 14.60387746471695
| Epoch (UTC): | 30 September 2022 23:26:22 |
| Eccentricity: | 0.0150279 |
| inclination: | 97.7988° |
| perigee height: | 585 km |
| apogee height: | 798 km |
| right ascension of ascending node: | 175.1103° |
| argument of perigee: | 72.2544° |
| revolutions per day: | 14.60387746 |
| mean anomaly at epoch: | 289.5012° |
| orbit number at epoch: | 47169 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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