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 40075U 26156.64818095 +.00000000 +00000-0 +23160-3 0 00005
2 40075 98.4034 128.8958 0003498 309.5091 50.5818 14.93500673 03
| Epoch (UTC): | 05 June 2026 15:33:22 |
| Eccentricity: | 0.0003498 |
| inclination: | 98.4034° |
| perigee height: | 585 km |
| apogee height: | 589 km |
| right ascension of ascending node: | 128.8958° |
| argument of perigee: | 309.5091° |
| revolutions per day: | 14.93500673 |
| mean anomaly at epoch: | 50.5818° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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