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 43678U 18084H 25317.15401535 .00006662 00000-0 55127-3 0 9994
2 43678 98.1067 139.4293 0007674 119.0035 241.1957 14.99231220383832
| Epoch (UTC): | 13 November 2025 03:41:46 |
| Eccentricity: | 0.0007674 |
| inclination: | 98.1067° |
| perigee height: | 564 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 139.4293° |
| argument of perigee: | 119.0035° |
| revolutions per day: | 14.99231220 |
| mean anomaly at epoch: | 241.1957° |
| orbit number at epoch: | 38383 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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