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 33412U 26145.63222137 +.00000000 +00000-0 +94955-4 0 00006
2 33412 97.8307 3.8283 0015424 348.0668 12.0192 15.06776181 01
| Epoch (UTC): | 25 May 2026 15:10:23 |
| Eccentricity: | 0.0015424 |
| inclination: | 97.8307° |
| perigee height: | 535 km |
| apogee height: | 557 km |
| right ascension of ascending node: | 3.8283° |
| argument of perigee: | 348.0668° |
| revolutions per day: | 15.06776181 |
| mean anomaly at epoch: | 12.0192° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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