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 17192U 26067.59422889 +.00000000 +00000-0 +70409-4 0 00005
2 17192 82.5077 143.1913 0016928 33.3298 85.5403 14.85913043 00
| Epoch (UTC): | 08 March 2026 14:15:41 |
| Eccentricity: | 0.0016928 |
| inclination: | 82.5077° |
| perigee height: | 599 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 143.1913° |
| argument of perigee: | 33.3298° |
| revolutions per day: | 14.85913043 |
| mean anomaly at epoch: | 85.5403° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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