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 63746U 26145.44326273 +.00000000 +00000-0 +30203-3 0 00009
2 63746 51.8994 146.1746 0000458 67.0005 293.1006 14.79935521 05
| Epoch (UTC): | 25 May 2026 10:38:17 |
| Eccentricity: | 0.0000458 |
| inclination: | 51.8994° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 146.1746° |
| argument of perigee: | 67.0005° |
| revolutions per day: | 14.79935521 |
| mean anomaly at epoch: | 293.1006° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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