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 43172U 26145.63502183 +.00000000 +00000-0 +19156-3 0 00001
2 43172 34.9972 288.4026 0002536 246.2354 113.8089 15.02593061 07
| Epoch (UTC): | 25 May 2026 15:14:25 |
| Eccentricity: | 0.0002536 |
| inclination: | 34.9972° |
| perigee height: | 557 km |
| apogee height: | 561 km |
| right ascension of ascending node: | 288.4026° |
| argument of perigee: | 246.2354° |
| revolutions per day: | 15.02593061 |
| mean anomaly at epoch: | 113.8089° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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