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 65826U 26145.21310904 +.00000000 +00000-0 +83361-2 0 00001
2 65826 53.1598 92.6050 0000984 85.9444 274.1671 15.33988764 09
| Epoch (UTC): | 25 May 2026 05:06:52 |
| Eccentricity: | 0.0000984 |
| inclination: | 53.1598° |
| perigee height: | 463 km |
| apogee height: | 465 km |
| right ascension of ascending node: | 92.6050° |
| argument of perigee: | 85.9444° |
| revolutions per day: | 15.33988764 |
| mean anomaly at epoch: | 274.1671° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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