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 43194U 26145.63576292 +.00000000 +00000-0 +27674-3 0 00001
2 43194 97.6855 310.8507 0015817 346.7866 13.2952 15.21023310 09
| Epoch (UTC): | 25 May 2026 15:15:29 |
| Eccentricity: | 0.0015817 |
| inclination: | 97.6855° |
| perigee height: | 492 km |
| apogee height: | 514 km |
| right ascension of ascending node: | 310.8507° |
| argument of perigee: | 346.7866° |
| revolutions per day: | 15.21023310 |
| mean anomaly at epoch: | 13.2952° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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