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 40032U 14033Y 23337.30253804 .00007800 00000-0 71333-3 0 9998
2 40032 97.9849 280.3845 0011963 90.2446 270.0145 14.95229738513224
| Epoch (UTC): | 03 December 2023 07:15:39 |
| Eccentricity: | 0.0011963 |
| inclination: | 97.9849° |
| perigee height: | 573 km |
| apogee height: | 590 km |
| right ascension of ascending node: | 280.3845° |
| argument of perigee: | 90.2446° |
| revolutions per day: | 14.95229738 |
| mean anomaly at epoch: | 270.0145° |
| orbit number at epoch: | 51322 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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