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 63750U 26145.37163586 +.00000000 +00000-0 +31607-3 0 00001
2 63750 51.9013 119.0159 0000683 50.1285 309.9737 14.79985714 09
| Epoch (UTC): | 25 May 2026 08:55:09 |
| Eccentricity: | 0.0000683 |
| inclination: | 51.9013° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 119.0159° |
| argument of perigee: | 50.1285° |
| revolutions per day: | 14.79985714 |
| mean anomaly at epoch: | 309.9737° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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