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 44549U 19063C 24357.58831869 .00001234 00000-0 41125-3 0 9990
2 44549 98.3791 15.0569 0039884 316.6059 43.1991 14.38847073274794
| Epoch (UTC): | 22 December 2024 14:07:10 |
| Eccentricity: | 0.0039884 |
| inclination: | 98.3791° |
| perigee height: | 734 km |
| apogee height: | 791 km |
| right ascension of ascending node: | 15.0569° |
| argument of perigee: | 316.6059° |
| revolutions per day: | 14.38847073 |
| mean anomaly at epoch: | 43.1991° |
| orbit number at epoch: | 27479 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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