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 65964U 26145.32683392 +.00000000 +00000-0 +17263-3 0 00009
2 65964 51.9009 4.1916 0000670 114.5514 245.5518 14.79933662 01
| Epoch (UTC): | 25 May 2026 07:50:38 |
| Eccentricity: | 0.0000670 |
| inclination: | 51.9009° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 4.1916° |
| argument of perigee: | 114.5514° |
| revolutions per day: | 14.79933662 |
| mean anomaly at epoch: | 245.5518° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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