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 44475U 26103.20878066 +.00000000 +00000-0 +00000-0 0 00006
2 44475 0.0219 147.0901 0001235 235.3168 36.6735 1.00272626 05
| Epoch (UTC): | 13 April 2026 05:00:38 |
| Eccentricity: | 0.0001235 |
| inclination: | 0.0219° |
| perigee height: | 35781 km |
| apogee height: | 35792 km |
| right ascension of ascending node: | 147.0901° |
| argument of perigee: | 235.3168° |
| revolutions per day: | 1.00272626 |
| mean anomaly at epoch: | 36.6735° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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