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 26074.28441932 +.00000000 +00000-0 +32957-3 0 00003
2 36596 97.7691 89.7840 0008338 67.1496 293.0616 15.15789027 03
| Epoch (UTC): | 15 March 2026 06:49:33 |
| Eccentricity: | 0.0008338 |
| inclination: | 97.7691° |
| perigee height: | 513 km |
| apogee height: | 524 km |
| right ascension of ascending node: | 89.7840° |
| argument of perigee: | 67.1496° |
| revolutions per day: | 15.15789027 |
| mean anomaly at epoch: | 293.0616° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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