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 44034U 26145.59144181 +.00000000 +00000-0 +00000-0 0 00009
2 44034 0.0664 124.1677 0004450 10.7655 0.1791 1.00270867 07
| Epoch (UTC): | 25 May 2026 14:11:40 |
| Eccentricity: | 0.0004450 |
| inclination: | 0.0664° |
| perigee height: | 35768 km |
| apogee height: | 35806 km |
| right ascension of ascending node: | 124.1677° |
| argument of perigee: | 10.7655° |
| revolutions per day: | 1.00270867 |
| mean anomaly at epoch: | 0.1791° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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