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 44333U 26145.56379500 +.00000000 +00000-0 +00000-0 0 00003
2 44333 0.0349 117.2235 0000641 128.7682 99.2706 1.00268949 03
| Epoch (UTC): | 25 May 2026 13:31:51 |
| Eccentricity: | 0.0000641 |
| inclination: | 0.0349° |
| perigee height: | 35785 km |
| apogee height: | 35790 km |
| right ascension of ascending node: | 117.2235° |
| argument of perigee: | 128.7682° |
| revolutions per day: | 1.00268949 |
| mean anomaly at epoch: | 99.2706° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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