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 26075.69356602 +.00000000 +00000-0 +47940-4 0 00007
2 16327 82.5368 343.0915 0016712 241.8270 157.1250 14.85821956 09
| Epoch (UTC): | 16 March 2026 16:38:44 |
| Eccentricity: | 0.0016712 |
| inclination: | 82.5368° |
| perigee height: | 599 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 343.0915° |
| argument of perigee: | 241.8270° |
| revolutions per day: | 14.85821956 |
| mean anomaly at epoch: | 157.1250° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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