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 43188U 26053.68595529 +.00000000 +00000-0 +39021-3 0 00000
2 43188 97.5460 319.4095 0010545 57.1033 303.1212 15.15410512 09
| Epoch (UTC): | 22 February 2026 16:27:46 |
| Eccentricity: | 0.0010545 |
| inclination: | 97.5460° |
| perigee height: | 512 km |
| apogee height: | 527 km |
| right ascension of ascending node: | 319.4095° |
| argument of perigee: | 57.1033° |
| revolutions per day: | 15.15410512 |
| mean anomaly at epoch: | 303.1212° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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