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 26067.06811683 +.00000000 +00000-0 +87466-4 0 00001
2 16327 82.5371 351.1841 0016583 273.1311 97.3297 14.85812737 04
| Epoch (UTC): | 08 March 2026 01:38:05 |
| Eccentricity: | 0.0016583 |
| inclination: | 82.5371° |
| perigee height: | 599 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 351.1841° |
| argument of perigee: | 273.1311° |
| revolutions per day: | 14.85812737 |
| mean anomaly at epoch: | 97.3297° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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