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 16182U 26129.85684762 +.00000000 +00000-0 +12507-3 0 00005
2 16182 71.0048 11.7775 0007240 180.2307 252.5132 14.16608654 03
| Epoch (UTC): | 09 May 2026 20:33:51 |
| Eccentricity: | 0.0007240 |
| inclination: | 71.0048° |
| perigee height: | 832 km |
| apogee height: | 842 km |
| right ascension of ascending node: | 11.7775° |
| argument of perigee: | 180.2307° |
| revolutions per day: | 14.16608654 |
| mean anomaly at epoch: | 252.5132° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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