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 26076.18826806 +.00000000 +00000-0 +11179-3 0 00003
2 16182 71.0014 124.7680 0009681 250.4589 166.3695 14.16598826 04
| Epoch (UTC): | 17 March 2026 04:31:06 |
| Eccentricity: | 0.0009681 |
| inclination: | 71.0014° |
| perigee height: | 830 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 124.7680° |
| argument of perigee: | 250.4589° |
| revolutions per day: | 14.16598826 |
| mean anomaly at epoch: | 166.3695° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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