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 19119U 26162.18456940 +.00000000 +00000-0 +13757-3 0 00004
2 19119 71.0037 49.3701 0009524 109.3599 16.9894 14.15758723 01
| Epoch (UTC): | 11 June 2026 04:25:46 |
| Eccentricity: | 0.0009524 |
| inclination: | 71.0037° |
| perigee height: | 833 km |
| apogee height: | 847 km |
| right ascension of ascending node: | 49.3701° |
| argument of perigee: | 109.3599° |
| revolutions per day: | 14.15758723 |
| mean anomaly at epoch: | 16.9894° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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