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 26032.27853333 +.00000000 +00000-0 +00000-0 0 00006
2 40732 2.8620 71.8183 0001042 235.8895 293.7522 1.00267887 00
| Epoch (UTC): | 01 February 2026 06:41:05 |
| Eccentricity: | 0.0001042 |
| inclination: | 2.8620° |
| perigee height: | 35783 km |
| apogee height: | 35792 km |
| right ascension of ascending node: | 71.8183° |
| argument of perigee: | 235.8895° |
| revolutions per day: | 1.00267887 |
| mean anomaly at epoch: | 293.7522° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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