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 43082U 26145.58519095 +.00000000 +00000-0 +20748-3 0 00004
2 43082 34.9952 287.8958 0004158 153.3692 206.7230 15.02565010 00
| Epoch (UTC): | 25 May 2026 14:02:40 |
| Eccentricity: | 0.0004158 |
| inclination: | 34.9952° |
| perigee height: | 556 km |
| apogee height: | 562 km |
| right ascension of ascending node: | 287.8958° |
| argument of perigee: | 153.3692° |
| revolutions per day: | 15.02565010 |
| mean anomaly at epoch: | 206.7230° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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