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 33396U 26145.63434265 +.00000000 +00000-0 +23164-3 0 00007
2 33396 98.5582 203.6490 0001325 85.5065 274.6263 14.20130911 09
| Epoch (UTC): | 25 May 2026 15:13:27 |
| Eccentricity: | 0.0001325 |
| inclination: | 98.5582° |
| perigee height: | 824 km |
| apogee height: | 826 km |
| right ascension of ascending node: | 203.6490° |
| argument of perigee: | 85.5065° |
| revolutions per day: | 14.20130911 |
| mean anomaly at epoch: | 274.6263° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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