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 32052U 26053.68020144 +.00000000 +00000-0 +28525-4 0 00002
2 32052 82.9791 290.2880 0037957 193.3791 166.6362 13.75156667 00
| Epoch (UTC): | 22 February 2026 16:19:29 |
| Eccentricity: | 0.0037957 |
| inclination: | 82.9791° |
| perigee height: | 953 km |
| apogee height: | 1009 km |
| right ascension of ascending node: | 290.2880° |
| argument of perigee: | 193.3791° |
| revolutions per day: | 13.75156667 |
| mean anomaly at epoch: | 166.6362° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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