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 53388U 26145.36318181 +.00000000 +00000-0 -20256-3 0 00008
2 53388 53.2128 139.9206 0001237 75.1376 284.9753 15.08860423 07
| Epoch (UTC): | 25 May 2026 08:42:58 |
| Eccentricity: | 0.0001237 |
| inclination: | 53.2128° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 139.9206° |
| argument of perigee: | 75.1376° |
| revolutions per day: | 15.08860423 |
| mean anomaly at epoch: | 284.9753° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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