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 26017.89614772 +.00000000 +00000-0 +27110-3 0 00007
2 19046 97.5112 1.3841 0028046 53.5771 306.8043 15.19165211 08
| Epoch (UTC): | 17 January 2026 21:30:27 |
| Eccentricity: | 0.0028046 |
| inclination: | 97.5112° |
| perigee height: | 489 km |
| apogee height: | 528 km |
| right ascension of ascending node: | 1.3841° |
| argument of perigee: | 53.5771° |
| revolutions per day: | 15.19165211 |
| mean anomaly at epoch: | 306.8043° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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