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 40119U 26145.27503137 +.00000000 +00000-0 +16598-3 0 00006
2 40119 97.9074 257.1032 0014023 179.8666 180.2560 14.94494037 03
| Epoch (UTC): | 25 May 2026 06:36:02 |
| Eccentricity: | 0.0014023 |
| inclination: | 97.9074° |
| perigee height: | 574 km |
| apogee height: | 594 km |
| right ascension of ascending node: | 257.1032° |
| argument of perigee: | 179.8666° |
| revolutions per day: | 14.94494037 |
| mean anomaly at epoch: | 180.2560° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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