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 17191U 26042.20918360 +.00000000 +00000-0 +47610-3 0 00006
2 17191 82.4605 122.9148 0002019 199.5515 160.5657 15.46675208 04
| Epoch (UTC): | 11 February 2026 05:01:13 |
| Eccentricity: | 0.0002019 |
| inclination: | 82.4605° |
| perigee height: | 425 km |
| apogee height: | 428 km |
| right ascension of ascending node: | 122.9148° |
| argument of perigee: | 199.5515° |
| revolutions per day: | 15.46675208 |
| mean anomaly at epoch: | 160.5657° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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