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 00050U 60009B 23343.46680140 -.00000096 00000-0 -95501-4 0 9995
2 00050 47.2283 139.5274 0113864 150.6705 210.0537 12.20136210825282
| Epoch (UTC): | 09 December 2023 11:12:11 |
| Eccentricity: | 0.0113864 |
| inclination: | 47.2283° |
| perigee height: | 1501 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 139.5274° |
| argument of perigee: | 150.6705° |
| revolutions per day: | 12.20136210 |
| mean anomaly at epoch: | 210.0537° |
| orbit number at epoch: | 82528 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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