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 38149U 99025EQW 24351.74249824 .00000935 00000-0 40158-3 0 9993
2 38149 98.3441 355.0606 0079085 141.9652 218.7148 14.25252969653446
| Epoch (UTC): | 16 December 2024 17:49:11 |
| Eccentricity: | 0.0079085 |
| inclination: | 98.3441° |
| perigee height: | 751 km |
| apogee height: | 864 km |
| right ascension of ascending node: | 355.0606° |
| argument of perigee: | 141.9652° |
| revolutions per day: | 14.25252969 |
| mean anomaly at epoch: | 218.7148° |
| orbit number at epoch: | 65344 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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