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 66047U 26145.23549669 +.00000000 +00000-0 +19628-3 0 00007
2 66047 89.0043 45.2549 0002002 70.4066 289.7301 13.51008991 02
| Epoch (UTC): | 25 May 2026 05:39:06 |
| Eccentricity: | 0.0002002 |
| inclination: | 89.0043° |
| perigee height: | 1067 km |
| apogee height: | 1070 km |
| right ascension of ascending node: | 45.2549° |
| argument of perigee: | 70.4066° |
| revolutions per day: | 13.51008991 |
| mean anomaly at epoch: | 289.7301° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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