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 32767U 26145.60987948 +.00000000 +00000-0 +00000-0 0 00007
2 32767 0.0131 2.3853 0001694 70.9869 161.3399 1.00272470 07
| Epoch (UTC): | 25 May 2026 14:38:13 |
| Eccentricity: | 0.0001694 |
| inclination: | 0.0131° |
| perigee height: | 35779 km |
| apogee height: | 35794 km |
| right ascension of ascending node: | 2.3853° |
| argument of perigee: | 70.9869° |
| revolutions per day: | 1.00272470 |
| mean anomaly at epoch: | 161.3399° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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