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 66046U 26145.44947170 +.00000000 +00000-0 +19318-3 0 00004
2 66046 89.0031 45.3934 0002137 75.9209 284.2179 13.51009504 09
| Epoch (UTC): | 25 May 2026 10:47:14 |
| Eccentricity: | 0.0002137 |
| inclination: | 89.0031° |
| perigee height: | 1067 km |
| apogee height: | 1070 km |
| right ascension of ascending node: | 45.3934° |
| argument of perigee: | 75.9209° |
| revolutions per day: | 13.51009504 |
| mean anomaly at epoch: | 284.2179° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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