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 26157.06900140 +.00000000 +00000-0 +51888-4 0 00007
2 16327 82.5335 266.6932 0017504 339.2549 193.6758 14.85885200 03
| Epoch (UTC): | 06 June 2026 01:39:21 |
| Eccentricity: | 0.0017504 |
| inclination: | 82.5335° |
| perigee height: | 599 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 266.6932° |
| argument of perigee: | 339.2549° |
| revolutions per day: | 14.85885200 |
| mean anomaly at epoch: | 193.6758° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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