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 66919U 26145.51327050 +.00000000 +00000-0 +67438-4 0 00007
2 66919 50.0067 227.2759 0001019 216.5331 143.5472 13.29336858 01
| Epoch (UTC): | 25 May 2026 12:19:06 |
| Eccentricity: | 0.0001019 |
| inclination: | 50.0067° |
| perigee height: | 1148 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 227.2759° |
| argument of perigee: | 216.5331° |
| revolutions per day: | 13.29336858 |
| mean anomaly at epoch: | 143.5472° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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