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 26017.93768563 +.00000000 +00000-0 +16080-3 0 00005
2 00047 66.6647 90.3620 0226031 248.9796 108.7001 14.45109079 04
| Epoch (UTC): | 17 January 2026 22:30:16 |
| Eccentricity: | 0.0226031 |
| inclination: | 66.6647° |
| perigee height: | 581 km |
| apogee height: | 903 km |
| right ascension of ascending node: | 90.3620° |
| argument of perigee: | 248.9796° |
| revolutions per day: | 14.45109079 |
| mean anomaly at epoch: | 108.7001° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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