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 32388U 26145.56916837 +.00000000 +00000-0 +00000-0 0 00000
2 32388 2.5461 80.8939 0003937 344.0964 309.2845 1.00272468 04
| Epoch (UTC): | 25 May 2026 13:39:36 |
| Eccentricity: | 0.0003937 |
| inclination: | 2.5461° |
| perigee height: | 35770 km |
| apogee height: | 35803 km |
| right ascension of ascending node: | 80.8939° |
| argument of perigee: | 344.0964° |
| revolutions per day: | 1.00272468 |
| mean anomaly at epoch: | 309.2845° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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