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 00047U 26140.98280705 +.00000000 +00000-0 +40890-4 0 00001
2 00047 66.6627 119.6873 0215765 159.7670 201.2156 14.45282955 04
| Epoch (UTC): | 20 May 2026 23:35:14 |
| Eccentricity: | 0.0215765 |
| inclination: | 66.6627° |
| perigee height: | 587 km |
| apogee height: | 895 km |
| right ascension of ascending node: | 119.6873° |
| argument of perigee: | 159.7670° |
| revolutions per day: | 14.45282955 |
| mean anomaly at epoch: | 201.2156° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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