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 26075.19969448 +.00000000 +00000-0 +79259-4 0 00007
2 16182 71.0016 126.8493 0009728 251.7146 165.1397 14.16598474 01
| Epoch (UTC): | 16 March 2026 04:47:33 |
| Eccentricity: | 0.0009728 |
| inclination: | 71.0016° |
| perigee height: | 830 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 126.8493° |
| argument of perigee: | 251.7146° |
| revolutions per day: | 14.16598474 |
| mean anomaly at epoch: | 165.1397° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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