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 65919U 26145.24037882 +.00000000 +00000-0 +56714-3 0 00001
2 65919 53.1574 169.7308 0001223 80.0133 280.1006 15.30208825 05
| Epoch (UTC): | 25 May 2026 05:46:08 |
| Eccentricity: | 0.0001223 |
| inclination: | 53.1574° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 169.7308° |
| argument of perigee: | 80.0133° |
| revolutions per day: | 15.30208825 |
| mean anomaly at epoch: | 280.1006° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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