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 16327U 26067.81700725 +.00000000 +00000-0 +78643-4 0 00005
2 16327 82.5369 350.4815 0016584 270.4246 143.3176 14.85813516 06
| Epoch (UTC): | 08 March 2026 19:36:29 |
| Eccentricity: | 0.0016584 |
| inclination: | 82.5369° |
| perigee height: | 599 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 350.4815° |
| argument of perigee: | 270.4246° |
| revolutions per day: | 14.85813516 |
| mean anomaly at epoch: | 143.3176° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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