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 41550U 26140.48428465 +.00000000 +00000-0 +00000-0 0 00002
2 41550 55.1019 222.4550 0003239 230.5838 129.4530 1.70473990 08
| Epoch (UTC): | 20 May 2026 11:37:22 |
| Eccentricity: | 0.0003239 |
| inclination: | 55.1019° |
| perigee height: | 23213 km |
| apogee height: | 23232 km |
| right ascension of ascending node: | 222.4550° |
| argument of perigee: | 230.5838° |
| revolutions per day: | 1.70473990 |
| mean anomaly at epoch: | 129.4530° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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