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 38992U 26145.58806178 +.00000000 +00000-0 +00000-0 0 00005
2 38992 0.0671 356.0393 0003001 68.2673 52.1656 1.00270158 01
| Epoch (UTC): | 25 May 2026 14:06:48 |
| Eccentricity: | 0.0003001 |
| inclination: | 0.0671° |
| perigee height: | 35774 km |
| apogee height: | 35800 km |
| right ascension of ascending node: | 356.0393° |
| argument of perigee: | 68.2673° |
| revolutions per day: | 1.00270158 |
| mean anomaly at epoch: | 52.1656° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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