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 38109U 12014A 24276.83364066 0.00000000 00000-0 00000-0 0 09
2 38109 123.0030 344.4999 0007644 347.6929 12.3071 13.41446539 09
| Epoch (UTC): | 02 October 2024 20:00:26 |
| Eccentricity: | 0.0007644 |
| inclination: | 123.0030° |
| perigee height: | 1098 km |
| apogee height: | 1109 km |
| right ascension of ascending node: | 344.4999° |
| argument of perigee: | 347.6929° |
| revolutions per day: | 13.41446539 |
| mean anomaly at epoch: | 12.3071° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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