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 40732U 26145.58554845 +.00000000 +00000-0 +00000-0 0 00001
2 40732 3.1455 71.2296 0001676 359.9886 32.0079 1.00273228 07
| Epoch (UTC): | 25 May 2026 14:03:11 |
| Eccentricity: | 0.0001676 |
| inclination: | 3.1455° |
| perigee height: | 35779 km |
| apogee height: | 35793 km |
| right ascension of ascending node: | 71.2296° |
| argument of perigee: | 359.9886° |
| revolutions per day: | 1.00273228 |
| mean anomaly at epoch: | 32.0079° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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