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 65555U 26145.41016316 +.00000000 +00000-0 +19082-3 0 00002
2 65555 49.9897 144.9589 0014249 236.9303 123.0268 14.84087944 01
| Epoch (UTC): | 25 May 2026 09:50:38 |
| Eccentricity: | 0.0014249 |
| inclination: | 49.9897° |
| perigee height: | 606 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 144.9589° |
| argument of perigee: | 236.9303° |
| revolutions per day: | 14.84087944 |
| mean anomaly at epoch: | 123.0268° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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