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 23340.43335895 .00003666 00000-0 50234-3 0 9998
2 40012 97.6822 146.2868 0053692 215.5115 144.2519 14.78045055509204
| Epoch (UTC): | 06 December 2023 10:24:02 |
| Eccentricity: | 0.0053692 |
| inclination: | 97.6822° |
| perigee height: | 598 km |
| apogee height: | 673 km |
| right ascension of ascending node: | 146.2868° |
| argument of perigee: | 215.5115° |
| revolutions per day: | 14.78045055 |
| mean anomaly at epoch: | 144.2519° |
| orbit number at epoch: | 50920 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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