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 63743U 26145.22302397 +.00000000 +00000-0 +22349-3 0 00005
2 63743 51.9002 132.1217 0000709 70.7140 289.3900 14.79926110 05
| Epoch (UTC): | 25 May 2026 05:21:09 |
| Eccentricity: | 0.0000709 |
| inclination: | 51.9002° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 132.1217° |
| argument of perigee: | 70.7140° |
| revolutions per day: | 14.79926110 |
| mean anomaly at epoch: | 289.3900° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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