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 43189U 26053.69910163 +.00000000 +00000-0 +35584-3 0 00007
2 43189 97.5477 319.4793 0011850 49.8344 310.3924 15.15368605 01
| Epoch (UTC): | 22 February 2026 16:46:42 |
| Eccentricity: | 0.0011850 |
| inclination: | 97.5477° |
| perigee height: | 512 km |
| apogee height: | 528 km |
| right ascension of ascending node: | 319.4793° |
| argument of perigee: | 49.8344° |
| revolutions per day: | 15.15368605 |
| mean anomaly at epoch: | 310.3924° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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