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 24252.13218762 .00008469 00000-0 13818-2 0 9990
2 39430 97.7186 121.4789 0138143 349.7148 10.1235 14.64955710575187
| Epoch (UTC): | 08 September 2024 03:10:21 |
| Eccentricity: | 0.0138143 |
| inclination: | 97.7186° |
| perigee height: | 580 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 121.4789° |
| argument of perigee: | 349.7148° |
| revolutions per day: | 14.64955710 |
| mean anomaly at epoch: | 10.1235° |
| orbit number at epoch: | 57518 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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