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 26129.77226005 +.00000000 +00000-0 +56601-4 0 00005
2 00047 66.6625 149.8168 0216859 168.0920 192.5435 14.45278112 02
| Epoch (UTC): | 09 May 2026 18:32:03 |
| Eccentricity: | 0.0216859 |
| inclination: | 66.6625° |
| perigee height: | 587 km |
| apogee height: | 896 km |
| right ascension of ascending node: | 149.8168° |
| argument of perigee: | 168.0920° |
| revolutions per day: | 14.45278112 |
| mean anomaly at epoch: | 192.5435° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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