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 38734U 26145.56722683 +.00000000 +00000-0 +63724-3 0 00000
2 38734 82.4740 78.9780 0017625 108.2050 252.0951 12.44902211 08
| Epoch (UTC): | 25 May 2026 13:36:48 |
| Eccentricity: | 0.0017625 |
| inclination: | 82.4740° |
| perigee height: | 1472 km |
| apogee height: | 1500 km |
| right ascension of ascending node: | 78.9780° |
| argument of perigee: | 108.2050° |
| revolutions per day: | 12.44902211 |
| mean anomaly at epoch: | 252.0951° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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