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 19039U 26105.48254715 +.00000000 +00000-0 +70465-4 0 00001
2 19039 74.0450 117.6146 0023980 213.7801 146.1828 14.39975598 04
| Epoch (UTC): | 15 April 2026 11:34:52 |
| Eccentricity: | 0.0023980 |
| inclination: | 74.0450° |
| perigee height: | 741 km |
| apogee height: | 776 km |
| right ascension of ascending node: | 117.6146° |
| argument of perigee: | 213.7801° |
| revolutions per day: | 14.39975598 |
| mean anomaly at epoch: | 146.1828° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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