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 32708U 26144.73974218 +.00000000 +00000-0 +00000-0 0 00001
2 32708 23.9746 20.7664 0048303 90.0743 96.0893 1.00349679 03
| Epoch (UTC): | 24 May 2026 17:45:13 |
| Eccentricity: | 0.0048303 |
| inclination: | 23.9746° |
| perigee height: | 35561 km |
| apogee height: | 35968 km |
| right ascension of ascending node: | 20.7664° |
| argument of perigee: | 90.0743° |
| revolutions per day: | 1.00349679 |
| mean anomaly at epoch: | 96.0893° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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