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 16792U 26128.14592764 +.00000000 +00000-0 +37166-4 0 00002
2 16792 82.4843 24.0089 0023998 34.7075 325.5701 14.85645108 01
| Epoch (UTC): | 08 May 2026 03:30:08 |
| Eccentricity: | 0.0023998 |
| inclination: | 82.4843° |
| perigee height: | 595 km |
| apogee height: | 628 km |
| right ascension of ascending node: | 24.0089° |
| argument of perigee: | 34.7075° |
| revolutions per day: | 14.85645108 |
| mean anomaly at epoch: | 325.5701° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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