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 26114.15311534 +.00000000 +00000-0 +15800-3 0 00000
2 33412 97.8347 331.8210 0017083 89.5778 270.7406 15.06596165 04
| Epoch (UTC): | 24 April 2026 03:40:29 |
| Eccentricity: | 0.0017083 |
| inclination: | 97.8347° |
| perigee height: | 535 km |
| apogee height: | 558 km |
| right ascension of ascending node: | 331.8210° |
| argument of perigee: | 89.5778° |
| revolutions per day: | 15.06596165 |
| mean anomaly at epoch: | 270.7406° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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