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 47269U 26145.56438359 +.00000000 +00000-0 +10320-2 0 00000
2 47269 87.8950 355.1693 0001836 88.5403 271.5936 13.12442882 03
| Epoch (UTC): | 25 May 2026 13:32:42 |
| Eccentricity: | 0.0001836 |
| inclination: | 87.8950° |
| perigee height: | 1212 km |
| apogee height: | 1215 km |
| right ascension of ascending node: | 355.1693° |
| argument of perigee: | 88.5403° |
| revolutions per day: | 13.12442882 |
| mean anomaly at epoch: | 271.5936° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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