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 26068.30032975 +.00000000 +00000-0 +73345-4 0 00009
2 16327 82.5369 350.0281 0016591 268.6761 208.7238 14.85813955 00
| Epoch (UTC): | 09 March 2026 07:12:28 |
| Eccentricity: | 0.0016591 |
| inclination: | 82.5369° |
| perigee height: | 599 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 350.0281° |
| argument of perigee: | 268.6761° |
| revolutions per day: | 14.85813955 |
| mean anomaly at epoch: | 208.7238° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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