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 26074.86937270 +.00000000 +00000-0 +65744-4 0 00002
2 16182 71.0017 127.5448 0009736 252.2081 280.5903 14.16598349 09
| Epoch (UTC): | 15 March 2026 20:51:53 |
| Eccentricity: | 0.0009736 |
| inclination: | 71.0017° |
| perigee height: | 830 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 127.5448° |
| argument of perigee: | 252.2081° |
| revolutions per day: | 14.16598349 |
| mean anomaly at epoch: | 280.5903° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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