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 37763U 26145.03150222 +.00000000 +00000-0 +00000-0 0 00002
2 37763 54.5939 165.8779 0158414 231.3629 308.9932 1.00289137 00
| Epoch (UTC): | 25 May 2026 00:45:21 |
| Eccentricity: | 0.0158414 |
| inclination: | 54.5939° |
| perigee height: | 35114 km |
| apogee height: | 36450 km |
| right ascension of ascending node: | 165.8779° |
| argument of perigee: | 231.3629° |
| revolutions per day: | 1.00289137 |
| mean anomaly at epoch: | 308.9932° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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