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 19460U 26032.48189632 +.00000000 +00000-0 +70151-4 0 00005
2 19460 84.9876 191.9351 0003544 151.3418 208.7971 14.34398975 09
| Epoch (UTC): | 01 February 2026 11:33:55 |
| Eccentricity: | 0.0003544 |
| inclination: | 84.9876° |
| perigee height: | 775 km |
| apogee height: | 780 km |
| right ascension of ascending node: | 191.9351° |
| argument of perigee: | 151.3418° |
| revolutions per day: | 14.34398975 |
| mean anomaly at epoch: | 208.7971° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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