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 40043U 14033AK 25140.69613350 .00001940 00000-0 24097-3 0 9996
2 40043 97.7336 296.6201 0050027 281.3192 78.2404 14.82863681587411
| Epoch (UTC): | 20 May 2025 16:42:25 |
| Eccentricity: | 0.0050027 |
| inclination: | 97.7336° |
| perigee height: | 585 km |
| apogee height: | 655 km |
| right ascension of ascending node: | 296.6201° |
| argument of perigee: | 281.3192° |
| revolutions per day: | 14.82863681 |
| mean anomaly at epoch: | 78.2404° |
| orbit number at epoch: | 58741 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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