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 53391U 26145.41838611 +.00000000 +00000-0 -12038-3 0 00002
2 53391 53.2114 139.6713 0000967 89.3647 270.7455 15.08850898 00
| Epoch (UTC): | 25 May 2026 10:02:28 |
| Eccentricity: | 0.0000967 |
| inclination: | 53.2114° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 139.6713° |
| argument of perigee: | 89.3647° |
| revolutions per day: | 15.08850898 |
| mean anomaly at epoch: | 270.7455° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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