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 40055U 26118.23036675 +.00000000 +00000-0 +13897-3 0 00008
2 40055 98.3192 351.6947 0012992 166.0914 194.0657 14.81171192 00
| Epoch (UTC): | 28 April 2026 05:31:43 |
| Eccentricity: | 0.0012992 |
| inclination: | 98.3192° |
| perigee height: | 617 km |
| apogee height: | 635 km |
| right ascension of ascending node: | 351.6947° |
| argument of perigee: | 166.0914° |
| revolutions per day: | 14.81171192 |
| mean anomaly at epoch: | 194.0657° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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