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 26021.19642587 +.00000000 +00000-0 +83140-3 0 00004
2 36596 97.7698 35.5057 0005318 235.5822 124.4907 15.15032954 08
| Epoch (UTC): | 21 January 2026 04:42:51 |
| Eccentricity: | 0.0005318 |
| inclination: | 97.7698° |
| perigee height: | 517 km |
| apogee height: | 525 km |
| right ascension of ascending node: | 35.5057° |
| argument of perigee: | 235.5822° |
| revolutions per day: | 15.15032954 |
| mean anomaly at epoch: | 124.4907° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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