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 44337U 26139.63539042 +.00000000 +00000-0 +00000-0 0 00007
2 44337 55.2397 159.1126 0039530 216.4700 210.4277 1.00275192 09
| Epoch (UTC): | 19 May 2026 15:14:57 |
| Eccentricity: | 0.0039530 |
| inclination: | 55.2397° |
| perigee height: | 35619 km |
| apogee height: | 35952 km |
| right ascension of ascending node: | 159.1126° |
| argument of perigee: | 216.4700° |
| revolutions per day: | 1.00275192 |
| mean anomaly at epoch: | 210.4277° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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