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 26087.83575065 +.00000000 +00000-0 +21436-3 0 00005
2 00047 66.6630 262.5198 0221041 198.7711 160.5153 14.45216522 00
| Epoch (UTC): | 28 March 2026 20:03:28 |
| Eccentricity: | 0.0221041 |
| inclination: | 66.6630° |
| perigee height: | 584 km |
| apogee height: | 899 km |
| right ascension of ascending node: | 262.5198° |
| argument of perigee: | 198.7711° |
| revolutions per day: | 14.45216522 |
| mean anomaly at epoch: | 160.5153° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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