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 26053.19022053 +.00000000 +00000-0 +18945-3 0 00005
2 41847 98.3917 130.2094 0343816 118.3498 245.2818 14.44411587 00
| Epoch (UTC): | 22 February 2026 04:33:55 |
| Eccentricity: | 0.0343816 |
| inclination: | 98.3917° |
| perigee height: | 499 km |
| apogee height: | 989 km |
| right ascension of ascending node: | 130.2094° |
| argument of perigee: | 118.3498° |
| revolutions per day: | 14.44411587 |
| mean anomaly at epoch: | 245.2818° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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