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 26145.24509514 +.00000000 +00000-0 +17346-3 0 00009
2 41847 98.3825 221.2420 0341711 198.9874 159.8318 14.44612230 09
| Epoch (UTC): | 25 May 2026 05:52:56 |
| Eccentricity: | 0.0341711 |
| inclination: | 98.3825° |
| perigee height: | 500 km |
| apogee height: | 987 km |
| right ascension of ascending node: | 221.2420° |
| argument of perigee: | 198.9874° |
| revolutions per day: | 14.44612230 |
| mean anomaly at epoch: | 159.8318° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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