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 32729U 26145.56414168 +.00000000 +00000-0 +00000-0 0 00009
2 32729 0.0101 118.8125 0000436 264.0904 324.1458 1.00272102 03
| Epoch (UTC): | 25 May 2026 13:32:21 |
| Eccentricity: | 0.0000436 |
| inclination: | 0.0101° |
| perigee height: | 35785 km |
| apogee height: | 35788 km |
| right ascension of ascending node: | 118.8125° |
| argument of perigee: | 264.0904° |
| revolutions per day: | 1.00272102 |
| mean anomaly at epoch: | 324.1458° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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