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 44071U 26145.66699369 +.00000000 +00000-0 +00000-0 0 00001
2 44071 0.0166 343.5190 0000489 34.9608 165.1869 1.00272154 05
| Epoch (UTC): | 25 May 2026 16:00:28 |
| Eccentricity: | 0.0000489 |
| inclination: | 0.0166° |
| perigee height: | 35784 km |
| apogee height: | 35789 km |
| right ascension of ascending node: | 343.5190° |
| argument of perigee: | 34.9608° |
| revolutions per day: | 1.00272154 |
| mean anomaly at epoch: | 165.1869° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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