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 26069.99343575 +.00000000 +00000-0 +38999-3 0 00001
2 36596 97.7699 85.3947 0008395 78.5722 281.6452 15.15729340 05
| Epoch (UTC): | 10 March 2026 23:50:32 |
| Eccentricity: | 0.0008395 |
| inclination: | 97.7699° |
| perigee height: | 513 km |
| apogee height: | 525 km |
| right ascension of ascending node: | 85.3947° |
| argument of perigee: | 78.5722° |
| revolutions per day: | 15.15729340 |
| mean anomaly at epoch: | 281.6452° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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