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 40024U 14033Q 24262.17554879 .00022587 00000-0 15257-2 0 9999
2 40024 98.0719 238.3737 0005153 185.9675 174.1490 15.06586402557239
| Epoch (UTC): | 18 September 2024 04:12:47 |
| Eccentricity: | 0.0005153 |
| inclination: | 98.0719° |
| perigee height: | 543 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 238.3737° |
| argument of perigee: | 185.9675° |
| revolutions per day: | 15.06586402 |
| mean anomaly at epoch: | 174.1490° |
| orbit number at epoch: | 55723 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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