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 19046U 26019.27935588 +.00000000 +00000-0 +29475-3 0 00008
2 19046 97.5117 2.7592 0027953 49.0445 311.3202 15.19182476 05
| Epoch (UTC): | 19 January 2026 06:42:16 |
| Eccentricity: | 0.0027953 |
| inclination: | 97.5117° |
| perigee height: | 489 km |
| apogee height: | 528 km |
| right ascension of ascending node: | 2.7592° |
| argument of perigee: | 49.0445° |
| revolutions per day: | 15.19182476 |
| mean anomaly at epoch: | 311.3202° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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