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 63344U 26145.56918373 +.00000000 +00000-0 +18892-3 0 00004
2 63344 97.6109 327.0575 0013400 227.8135 132.1958 15.10843404 08
| Epoch (UTC): | 25 May 2026 13:39:37 |
| Eccentricity: | 0.0013400 |
| inclination: | 97.6109° |
| perigee height: | 524 km |
| apogee height: | 543 km |
| right ascension of ascending node: | 327.0575° |
| argument of perigee: | 227.8135° |
| revolutions per day: | 15.10843404 |
| mean anomaly at epoch: | 132.1958° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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