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 26135.30833757 +.00000000 +00000-0 +44686-4 0 00009
2 00047 66.6625 134.9380 0216316 163.9896 196.8193 14.45280644 08
| Epoch (UTC): | 15 May 2026 07:24:00 |
| Eccentricity: | 0.0216316 |
| inclination: | 66.6625° |
| perigee height: | 587 km |
| apogee height: | 895 km |
| right ascension of ascending node: | 134.9380° |
| argument of perigee: | 163.9896° |
| revolutions per day: | 14.45280644 |
| mean anomaly at epoch: | 196.8193° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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