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 53405U 26145.36686869 +.00000000 +00000-0 -62843-4 0 00008
2 53405 53.2124 139.9035 0001109 90.0826 270.0293 15.08847048 00
| Epoch (UTC): | 25 May 2026 08:48:17 |
| Eccentricity: | 0.0001109 |
| inclination: | 53.2124° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 139.9035° |
| argument of perigee: | 90.0826° |
| revolutions per day: | 15.08847048 |
| mean anomaly at epoch: | 270.0293° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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