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 19649U 26159.03891564 +.00000000 +00000-0 -16722-4 0 00004
2 19649 71.0004 24.2911 0005406 349.0064 11.0940 14.15213869 08
| Epoch (UTC): | 08 June 2026 00:56:02 |
| Eccentricity: | 0.0005406 |
| inclination: | 71.0004° |
| perigee height: | 838 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 24.2911° |
| argument of perigee: | 349.0064° |
| revolutions per day: | 14.15213869 |
| mean anomaly at epoch: | 11.0940° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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