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 44071U 26145.59568847 +.00000000 +00000-0 +00000-0 0 00009
2 44071 0.0166 342.7317 0000487 35.5041 139.6906 1.00272135 00
| Epoch (UTC): | 25 May 2026 14:17:47 |
| Eccentricity: | 0.0000487 |
| inclination: | 0.0166° |
| perigee height: | 35784 km |
| apogee height: | 35789 km |
| right ascension of ascending node: | 342.7317° |
| argument of perigee: | 35.5041° |
| revolutions per day: | 1.00272135 |
| mean anomaly at epoch: | 139.6906° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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