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 26155.30809252 +.00000000 +00000-0 +00000-0 0 00005
2 44475 0.0051 329.5990 0001290 131.4598 45.1173 1.00271396 02
| Epoch (UTC): | 04 June 2026 07:23:39 |
| Eccentricity: | 0.0001290 |
| inclination: | 0.0051° |
| perigee height: | 35781 km |
| apogee height: | 35792 km |
| right ascension of ascending node: | 329.5990° |
| argument of perigee: | 131.4598° |
| revolutions per day: | 1.00271396 |
| mean anomaly at epoch: | 45.1173° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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