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 19274U 26039.15670285 +.00000000 +00000-0 +35571-3 0 00004
2 19274 82.4703 292.9560 0011366 282.6182 77.3788 15.31057545 04
| Epoch (UTC): | 08 February 2026 03:45:39 |
| Eccentricity: | 0.0011366 |
| inclination: | 82.4703° |
| perigee height: | 465 km |
| apogee height: | 480 km |
| right ascension of ascending node: | 292.9560° |
| argument of perigee: | 282.6182° |
| revolutions per day: | 15.31057545 |
| mean anomaly at epoch: | 77.3788° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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