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 39265U 26106.20360319 +.00000000 +00000-0 +19699-3 0 00004
2 39265 80.9145 141.7427 0304384 270.4798 86.1566 15.21337906 08
| Epoch (UTC): | 16 April 2026 04:53:11 |
| Eccentricity: | 0.0304384 |
| inclination: | 80.9145° |
| perigee height: | 292 km |
| apogee height: | 711 km |
| right ascension of ascending node: | 141.7427° |
| argument of perigee: | 270.4798° |
| revolutions per day: | 15.21337906 |
| mean anomaly at epoch: | 86.1566° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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