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 26150.78633175 +.00000000 +00000-0 +27072-3 0 00002
2 41847 98.3824 226.7206 0342018 182.1768 177.7955 14.44632524 02
| Epoch (UTC): | 30 May 2026 18:52:19 |
| Eccentricity: | 0.0342018 |
| inclination: | 98.3824° |
| perigee height: | 500 km |
| apogee height: | 987 km |
| right ascension of ascending node: | 226.7206° |
| argument of perigee: | 182.1768° |
| revolutions per day: | 14.44632524 |
| mean anomaly at epoch: | 177.7955° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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