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 40032U 26145.44565574 +.00000000 +00000-0 +34874-3 0 00009
2 40032 98.0754 140.9170 0005769 247.4865 112.5755 15.14817614 03
| Epoch (UTC): | 25 May 2026 10:41:44 |
| Eccentricity: | 0.0005769 |
| inclination: | 98.0754° |
| perigee height: | 518 km |
| apogee height: | 526 km |
| right ascension of ascending node: | 140.9170° |
| argument of perigee: | 247.4865° |
| revolutions per day: | 15.14817614 |
| mean anomaly at epoch: | 112.5755° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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