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 39679U 14021B 23150.36013872 .00005449 00000-0 24471-3 0 9996
2 39679 51.6099 136.3671 0154668 87.6300 274.2371 15.12746826501540
| Epoch (UTC): | 30 May 2023 08:38:35 |
| Eccentricity: | 0.0154668 |
| inclination: | 51.6099° |
| perigee height: | 421 km |
| apogee height: | 634 km |
| right ascension of ascending node: | 136.3671° |
| argument of perigee: | 87.6300° |
| revolutions per day: | 15.12746826 |
| mean anomaly at epoch: | 274.2371° |
| orbit number at epoch: | 50154 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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