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 24280.17015196 .00031772 00000-0 20927-2 0 9999
2 40024 98.0744 257.2409 0007521 135.4867 224.6965 15.07428601560461
| Epoch (UTC): | 06 October 2024 04:05:01 |
| Eccentricity: | 0.0007521 |
| inclination: | 98.0744° |
| perigee height: | 539 km |
| apogee height: | 549 km |
| right ascension of ascending node: | 257.2409° |
| argument of perigee: | 135.4867° |
| revolutions per day: | 15.07428601 |
| mean anomaly at epoch: | 224.6965° |
| orbit number at epoch: | 56046 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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