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 41847U 26099.18396691 +.00000000 +00000-0 +12622-3 0 00002
2 41847 98.3844 175.6955 0341827 339.1224 19.6284 14.44548755 06
| Epoch (UTC): | 09 April 2026 04:24:54 |
| Eccentricity: | 0.0341827 |
| inclination: | 98.3844° |
| perigee height: | 500 km |
| apogee height: | 987 km |
| right ascension of ascending node: | 175.6955° |
| argument of perigee: | 339.1224° |
| revolutions per day: | 14.44548755 |
| mean anomaly at epoch: | 19.6284° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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