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 is defined by the following mean orbital elements,
1 38014U 26145.59222181 +.00000000 +00000-0 +00000-0 0 00007
2 38014 0.0525 118.6506 0002260 238.0997 142.1558 1.00275190 06
| Epoch (UTC): | 25 May 2026 14:12:47 |
| Eccentricity: | 0.0002260 |
| inclination: | 0.0525° |
| perigee height: | 35776 km |
| apogee height: | 35795 km |
| right ascension of ascending node: | 118.6506° |
| argument of perigee: | 238.0997° |
| revolutions per day: | 1.00275190 |
| mean anomaly at epoch: | 142.1558° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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