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 41180U 26140.10616814 +.00000000 +00000-0 +83822-4 0 00004
2 41180 47.0015 44.1258 0000607 185.1438 174.9442 14.58763467 02
| Epoch (UTC): | 20 May 2026 02:32:52 |
| Eccentricity: | 0.0000607 |
| inclination: | 47.0015° |
| perigee height: | 697 km |
| apogee height: | 698 km |
| right ascension of ascending node: | 44.1258° |
| argument of perigee: | 185.1438° |
| revolutions per day: | 14.58763467 |
| mean anomaly at epoch: | 174.9442° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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