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 37839U 11058B 24279.88468365 .00001666 00000-0 73365-3 0 9993
2 37839 19.9600 109.9251 0018723 78.4034 310.0788 14.13350421671400
| Epoch (UTC): | 05 October 2024 21:13:56 |
| Eccentricity: | 0.0018723 |
| inclination: | 19.9600° |
| perigee height: | 834 km |
| apogee height: | 861 km |
| right ascension of ascending node: | 109.9251° |
| argument of perigee: | 78.4034° |
| revolutions per day: | 14.13350421 |
| mean anomaly at epoch: | 310.0788° |
| orbit number at epoch: | 67140 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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