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 46U 60007B 25168.18828677 .00000421 00000-0 97958-4 0 9991
2 46 66.6870 142.6396 0200916 209.4977 149.4679 14.54002560403905
| Epoch (UTC): | 17 June 2025 04:31:07 |
| Eccentricity: | 0.0200916 |
| inclination: | 66.6870° |
| perigee height: | 570 km |
| apogee height: | 855 km |
| right ascension of ascending node: | 142.6396° |
| argument of perigee: | 209.4977° |
| revolutions per day: | 14.54002560 |
| mean anomaly at epoch: | 149.4679° |
| orbit number at epoch: | 40390 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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