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 37191U 26145.44002818 +.00000000 +00000-0 +81482-4 0 00006
2 37191 51.9954 237.0320 0003088 132.9175 308.3555 11.67547255 02
| Epoch (UTC): | 25 May 2026 10:33:38 |
| Eccentricity: | 0.0003088 |
| inclination: | 51.9954° |
| perigee height: | 1827 km |
| apogee height: | 1832 km |
| right ascension of ascending node: | 237.0320° |
| argument of perigee: | 132.9175° |
| revolutions per day: | 11.67547255 |
| mean anomaly at epoch: | 308.3555° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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