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 65553U 26145.28005911 +.00000000 +00000-0 +14698-3 0 00002
2 65553 49.9842 146.1958 0008083 185.1860 174.8996 14.84130301 03
| Epoch (UTC): | 25 May 2026 06:43:17 |
| Eccentricity: | 0.0008083 |
| inclination: | 49.9842° |
| perigee height: | 611 km |
| apogee height: | 622 km |
| right ascension of ascending node: | 146.1958° |
| argument of perigee: | 185.1860° |
| revolutions per day: | 14.84130301 |
| mean anomaly at epoch: | 174.8996° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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