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 26067.22070733 +.00000000 +00000-0 +45621-3 0 00008
2 36596 97.7697 82.5583 0008576 86.2494 273.9718 15.15688513 06
| Epoch (UTC): | 08 March 2026 05:17:49 |
| Eccentricity: | 0.0008576 |
| inclination: | 97.7697° |
| perigee height: | 513 km |
| apogee height: | 525 km |
| right ascension of ascending node: | 82.5583° |
| argument of perigee: | 86.2494° |
| revolutions per day: | 15.15688513 |
| mean anomaly at epoch: | 273.9718° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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