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 63744U 26145.61503250 +.00000000 +00000-0 +26819-3 0 00006
2 63744 51.9002 114.0697 0001649 46.1704 313.9393 14.76383289 05
| Epoch (UTC): | 25 May 2026 14:45:38 |
| Eccentricity: | 0.0001649 |
| inclination: | 51.9002° |
| perigee height: | 640 km |
| apogee height: | 642 km |
| right ascension of ascending node: | 114.0697° |
| argument of perigee: | 46.1704° |
| revolutions per day: | 14.76383289 |
| mean anomaly at epoch: | 313.9393° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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