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 19306U 26066.25578442 +.00000000 +00000-0 +65425-3 0 00004
2 19306 102.2114 176.0675 0145090 229.9265 157.3123 12.15446585 01
| Epoch (UTC): | 07 March 2026 06:08:19 |
| Eccentricity: | 0.0145090 |
| inclination: | 102.2114° |
| perigee height: | 1497 km |
| apogee height: | 1728 km |
| right ascension of ascending node: | 176.0675° |
| argument of perigee: | 229.9265° |
| revolutions per day: | 12.15446585 |
| mean anomaly at epoch: | 157.3123° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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