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 44311U 26145.39490803 +.00000000 +00000-0 +27343-3 0 00002
2 44311 44.9692 134.5188 0025105 199.9971 159.9930 15.27255788 03
| Epoch (UTC): | 25 May 2026 09:28:40 |
| Eccentricity: | 0.0025105 |
| inclination: | 44.9692° |
| perigee height: | 467 km |
| apogee height: | 501 km |
| right ascension of ascending node: | 134.5188° |
| argument of perigee: | 199.9971° |
| revolutions per day: | 15.27255788 |
| mean anomaly at epoch: | 159.9930° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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