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 36596U 26042.26293041 +.00000000 +00000-0 +36406-3 0 00005
2 36596 97.7706 57.0374 0007330 156.8313 203.3250 15.15361694 09
| Epoch (UTC): | 11 February 2026 06:18:37 |
| Eccentricity: | 0.0007330 |
| inclination: | 97.7706° |
| perigee height: | 515 km |
| apogee height: | 525 km |
| right ascension of ascending node: | 57.0374° |
| argument of perigee: | 156.8313° |
| revolutions per day: | 15.15361694 |
| mean anomaly at epoch: | 203.3250° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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