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 40076U 26134.95913950 +.00000000 +00000-0 +30772-3 0 00009
2 40076 98.3809 123.8963 0007162 35.5867 324.5837 15.12751702 01
| Epoch (UTC): | 14 May 2026 23:01:09 |
| Eccentricity: | 0.0007162 |
| inclination: | 98.3809° |
| perigee height: | 523 km |
| apogee height: | 533 km |
| right ascension of ascending node: | 123.8963° |
| argument of perigee: | 35.5867° |
| revolutions per day: | 15.12751702 |
| mean anomaly at epoch: | 324.5837° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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