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 26064.68944376 +.00000000 +00000-0 -21638-4 0 00001
2 16182 71.0035 148.9756 0009962 264.5817 208.5938 14.16599681 00
| Epoch (UTC): | 05 March 2026 16:32:47 |
| Eccentricity: | 0.0009962 |
| inclination: | 71.0035° |
| perigee height: | 830 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 148.9756° |
| argument of perigee: | 264.5817° |
| revolutions per day: | 14.16599681 |
| mean anomaly at epoch: | 208.5938° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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