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 45376U 26145.26755602 +.00000000 +00000-0 +10235-2 0 00002
2 45376 53.0418 139.3563 0006175 27.0698 333.0635 15.60808819 08
| Epoch (UTC): | 25 May 2026 06:25:16 |
| Eccentricity: | 0.0006175 |
| inclination: | 53.0418° |
| perigee height: | 381 km |
| apogee height: | 389 km |
| right ascension of ascending node: | 139.3563° |
| argument of perigee: | 27.0698° |
| revolutions per day: | 15.60808819 |
| mean anomaly at epoch: | 333.0635° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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