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 47374U 26145.66668980 +.00000000 +00000-0 +69967-3 0 00005
2 47374 53.0455 22.3668 0003790 115.3301 271.4878 15.85059912 01
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0003790 |
| inclination: | 53.0455° |
| perigee height: | 314 km |
| apogee height: | 319 km |
| right ascension of ascending node: | 22.3668° |
| argument of perigee: | 115.3301° |
| revolutions per day: | 15.85059912 |
| mean anomaly at epoch: | 271.4878° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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