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 63440U 26145.26078152 +.00000000 +00000-0 +53133-3 0 00007
2 63440 53.1583 144.2856 0000965 82.2383 277.8732 15.42171730 07
| Epoch (UTC): | 25 May 2026 06:15:31 |
| Eccentricity: | 0.0000965 |
| inclination: | 53.1583° |
| perigee height: | 439 km |
| apogee height: | 440 km |
| right ascension of ascending node: | 144.2856° |
| argument of perigee: | 82.2383° |
| revolutions per day: | 15.42171730 |
| mean anomaly at epoch: | 277.8732° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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