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 26076.17920387 +.00000000 +00000-0 +46988-4 0 00009
2 16327 82.5369 342.6359 0016736 240.0961 234.9052 14.85822347 00
| Epoch (UTC): | 17 March 2026 04:18:03 |
| Eccentricity: | 0.0016736 |
| inclination: | 82.5369° |
| perigee height: | 599 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 342.6359° |
| argument of perigee: | 240.0961° |
| revolutions per day: | 14.85822347 |
| mean anomaly at epoch: | 234.9052° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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