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 41182U 26145.16082419 +.00000000 +00000-0 +17108-3 0 00008
2 41182 47.0010 110.3134 0003761 319.8741 40.1867 14.58838006 02
| Epoch (UTC): | 25 May 2026 03:51:35 |
| Eccentricity: | 0.0003761 |
| inclination: | 47.0010° |
| perigee height: | 694 km |
| apogee height: | 700 km |
| right ascension of ascending node: | 110.3134° |
| argument of perigee: | 319.8741° |
| revolutions per day: | 14.58838006 |
| mean anomaly at epoch: | 40.1867° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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