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 26065.38731163 +.00000000 +00000-0 -37693-4 0 00005
2 16182 71.0034 147.5065 0009968 263.7562 167.3141 14.16599577 03
| Epoch (UTC): | 06 March 2026 09:17:43 |
| Eccentricity: | 0.0009968 |
| inclination: | 71.0034° |
| perigee height: | 830 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 147.5065° |
| argument of perigee: | 263.7562° |
| revolutions per day: | 14.16599577 |
| mean anomaly at epoch: | 167.3141° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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