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 26040.21590330 +.00000000 +00000-0 +32899-3 0 00001
2 36596 97.7709 54.9446 0007154 162.6819 197.4658 15.15336256 09
| Epoch (UTC): | 09 February 2026 05:10:54 |
| Eccentricity: | 0.0007154 |
| inclination: | 97.7709° |
| perigee height: | 515 km |
| apogee height: | 525 km |
| right ascension of ascending node: | 54.9446° |
| argument of perigee: | 162.6819° |
| revolutions per day: | 15.15336256 |
| mean anomaly at epoch: | 197.4658° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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