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 40012U 14033C 23333.46024642 .00005785 00000-0 79009-3 0 9993
2 40012 97.6821 139.6341 0053438 238.5784 121.0196 14.77968818508179
| Epoch (UTC): | 29 November 2023 11:02:45 |
| Eccentricity: | 0.0053438 |
| inclination: | 97.6821° |
| perigee height: | 598 km |
| apogee height: | 673 km |
| right ascension of ascending node: | 139.6341° |
| argument of perigee: | 238.5784° |
| revolutions per day: | 14.77968818 |
| mean anomaly at epoch: | 121.0196° |
| orbit number at epoch: | 50817 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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