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 47286U 26145.55590339 +.00000000 +00000-0 +46804-3 0 00002
2 47286 87.8962 355.1425 0001801 80.2919 279.8413 13.12442913 07
| Epoch (UTC): | 25 May 2026 13:20:30 |
| Eccentricity: | 0.0001801 |
| inclination: | 87.8962° |
| perigee height: | 1212 km |
| apogee height: | 1215 km |
| right ascension of ascending node: | 355.1425° |
| argument of perigee: | 80.2919° |
| revolutions per day: | 13.12442913 |
| mean anomaly at epoch: | 279.8413° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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