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 23149.96376245 .00005418 00000-0 24344-3 0 9991
2 39679 51.6099 138.2247 0154676 86.2495 275.6148 15.12742496501804
| Epoch (UTC): | 29 May 2023 23:07:49 |
| Eccentricity: | 0.0154676 |
| inclination: | 51.6099° |
| perigee height: | 421 km |
| apogee height: | 634 km |
| right ascension of ascending node: | 138.2247° |
| argument of perigee: | 86.2495° |
| revolutions per day: | 15.12742496 |
| mean anomaly at epoch: | 275.6148° |
| orbit number at epoch: | 50180 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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