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 26162.14705390 +.00000000 +00000-0 -80148-4 0 00003
2 16182 71.0037 303.7943 0005497 123.8776 53.0679 14.16611816 01
| Epoch (UTC): | 11 June 2026 03:31:45 |
| Eccentricity: | 0.0005497 |
| inclination: | 71.0037° |
| perigee height: | 833 km |
| apogee height: | 841 km |
| right ascension of ascending node: | 303.7943° |
| argument of perigee: | 123.8776° |
| revolutions per day: | 14.16611816 |
| mean anomaly at epoch: | 53.0679° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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