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 26150.49580486 +.00000000 +00000-0 +23585-3 0 00001
2 33396 98.5585 208.3528 0001316 87.4248 272.7080 14.20131645 01
| Epoch (UTC): | 30 May 2026 11:53:57 |
| Eccentricity: | 0.0001316 |
| inclination: | 98.5585° |
| perigee height: | 824 km |
| apogee height: | 826 km |
| right ascension of ascending node: | 208.3528° |
| argument of perigee: | 87.4248° |
| revolutions per day: | 14.20131645 |
| mean anomaly at epoch: | 272.7080° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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