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 26156.70767861 +.00000000 +00000-0 +00000-0 0 00001
2 40732 3.1737 71.1731 0001660 4.4419 82.6651 1.00276730 08
| Epoch (UTC): | 05 June 2026 16:59:03 |
| Eccentricity: | 0.0001660 |
| inclination: | 3.1737° |
| perigee height: | 35778 km |
| apogee height: | 35792 km |
| right ascension of ascending node: | 71.1731° |
| argument of perigee: | 4.4419° |
| revolutions per day: | 1.00276730 |
| mean anomaly at epoch: | 82.6651° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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