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 23225.09327980 0.00000000 00000-0 00000-0 0 04
2 38109 123.0025 131.1884 0003410 70.8461 289.1538 13.41447886 08
| Epoch (UTC): | 13 August 2023 02:14:19 |
| Eccentricity: | 0.0003410 |
| inclination: | 123.0025° |
| perigee height: | 1101 km |
| apogee height: | 1106 km |
| right ascension of ascending node: | 131.1884° |
| argument of perigee: | 70.8461° |
| revolutions per day: | 13.41447886 |
| mean anomaly at epoch: | 289.1538° |
| 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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