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 24255.61286943 .00017361 00000-0 13800-2 0 9999
2 40032 98.0100 210.4696 0007994 191.2764 168.8281 15.00484991555624
| Epoch (UTC): | 11 September 2024 14:42:31 |
| Eccentricity: | 0.0007994 |
| inclination: | 98.0100° |
| perigee height: | 560 km |
| apogee height: | 571 km |
| right ascension of ascending node: | 210.4696° |
| argument of perigee: | 191.2764° |
| revolutions per day: | 15.00484991 |
| mean anomaly at epoch: | 168.8281° |
| orbit number at epoch: | 55562 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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