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 26020.60200072 +.00000000 +00000-0 +16358-2 0 00004
2 36596 97.7696 34.8984 0005293 236.9393 123.1330 15.15042071 04
| Epoch (UTC): | 20 January 2026 14:26:52 |
| Eccentricity: | 0.0005293 |
| inclination: | 97.7696° |
| perigee height: | 517 km |
| apogee height: | 525 km |
| right ascension of ascending node: | 34.8984° |
| argument of perigee: | 236.9393° |
| revolutions per day: | 15.15042071 |
| mean anomaly at epoch: | 123.1330° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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