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 45375U 26145.24306332 +.00000000 +00000-0 +44085-3 0 00002
2 45375 53.0454 138.6237 0005520 27.1332 332.9970 15.65675954 03
| Epoch (UTC): | 25 May 2026 05:50:00 |
| Eccentricity: | 0.0005520 |
| inclination: | 53.0454° |
| perigee height: | 368 km |
| apogee height: | 375 km |
| right ascension of ascending node: | 138.6237° |
| argument of perigee: | 27.1332° |
| revolutions per day: | 15.65675954 |
| mean anomaly at epoch: | 332.9970° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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