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 63850U 26145.61744753 +.00000000 +00000-0 +53958-3 0 00003
2 63850 43.0029 3.7706 0003444 283.3407 76.7060 15.27588691 05
| Epoch (UTC): | 25 May 2026 14:49:07 |
| Eccentricity: | 0.0003444 |
| inclination: | 43.0029° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 3.7706° |
| argument of perigee: | 283.3407° |
| revolutions per day: | 15.27588691 |
| mean anomaly at epoch: | 76.7060° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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