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 23333.05403350 .00005490 00000-0 75033-3 0 9991
2 40012 97.6820 139.2465 0053433 239.8894 119.7015 14.77963566508115
| Epoch (UTC): | 29 November 2023 01:17:48 |
| Eccentricity: | 0.0053433 |
| inclination: | 97.6820° |
| perigee height: | 598 km |
| apogee height: | 673 km |
| right ascension of ascending node: | 139.2465° |
| argument of perigee: | 239.8894° |
| revolutions per day: | 14.77963566 |
| mean anomaly at epoch: | 119.7015° |
| orbit number at epoch: | 50811 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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