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 26079.88208977 +.00000000 +00000-0 +41644-3 0 00003
2 39265 80.9184 173.4798 0311953 358.9006 1.1495 15.19564179 07
| Epoch (UTC): | 20 March 2026 21:10:12 |
| Eccentricity: | 0.0311953 |
| inclination: | 80.9184° |
| perigee height: | 292 km |
| apogee height: | 722 km |
| right ascension of ascending node: | 173.4798° |
| argument of perigee: | 358.9006° |
| revolutions per day: | 15.19564179 |
| mean anomaly at epoch: | 1.1495° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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