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 63740U 26145.10418329 +.00000000 +00000-0 +16251-3 0 00007
2 63740 51.9009 117.6869 0000672 62.8374 297.2657 14.79943884 04
| Epoch (UTC): | 25 May 2026 02:30:01 |
| Eccentricity: | 0.0000672 |
| inclination: | 51.9009° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 117.6869° |
| argument of perigee: | 62.8374° |
| revolutions per day: | 14.79943884 |
| mean anomaly at epoch: | 297.2657° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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