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 40042U 14033AJ 24277.91147355 .00037425 00000-0 25090-2 0 9997
2 40042 98.0821 247.0103 0015101 118.9232 241.3511 15.06662954559180
| Epoch (UTC): | 03 October 2024 21:52:31 |
| Eccentricity: | 0.0015101 |
| inclination: | 98.0821° |
| perigee height: | 536 km |
| apogee height: | 557 km |
| right ascension of ascending node: | 247.0103° |
| argument of perigee: | 118.9232° |
| revolutions per day: | 15.06662954 |
| mean anomaly at epoch: | 241.3511° |
| orbit number at epoch: | 55918 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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