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 26140.74758332 +.00000000 +00000-0 +00000-0 0 00001
2 44071 0.0147 335.3490 0000502 345.0017 247.4847 1.00271511 08
| Epoch (UTC): | 20 May 2026 17:56:31 |
| Eccentricity: | 0.0000502 |
| inclination: | 0.0147° |
| perigee height: | 35785 km |
| apogee height: | 35789 km |
| right ascension of ascending node: | 335.3490° |
| argument of perigee: | 345.0017° |
| revolutions per day: | 1.00271511 |
| mean anomaly at epoch: | 247.4847° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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