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 39763U 26145.59932476 +.00000000 +00000-0 +66371-3 0 00000
2 39763 82.4437 123.0569 0022262 120.6841 239.6437 12.42979679 00
| Epoch (UTC): | 25 May 2026 14:23:01 |
| Eccentricity: | 0.0022262 |
| inclination: | 82.4437° |
| perigee height: | 1476 km |
| apogee height: | 1512 km |
| right ascension of ascending node: | 123.0569° |
| argument of perigee: | 120.6841° |
| revolutions per day: | 12.42979679 |
| mean anomaly at epoch: | 239.6437° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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