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 26106.64494056 +.00000000 +00000-0 +10659-3 0 00008
2 16182 71.0032 60.6425 0008552 213.3013 319.1399 14.16606259 04
| Epoch (UTC): | 16 April 2026 15:28:42 |
| Eccentricity: | 0.0008552 |
| inclination: | 71.0032° |
| perigee height: | 831 km |
| apogee height: | 843 km |
| right ascension of ascending node: | 60.6425° |
| argument of perigee: | 213.3013° |
| revolutions per day: | 14.16606259 |
| mean anomaly at epoch: | 319.1399° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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