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 65571U 26145.66195413 +.00000000 +00000-0 +69133-4 0 00006
2 65571 81.3023 31.6605 0005025 261.4783 98.5804 13.83813737 05
| Epoch (UTC): | 25 May 2026 15:53:12 |
| Eccentricity: | 0.0005025 |
| inclination: | 81.3023° |
| perigee height: | 947 km |
| apogee height: | 954 km |
| right ascension of ascending node: | 31.6605° |
| argument of perigee: | 261.4783° |
| revolutions per day: | 13.83813737 |
| mean anomaly at epoch: | 98.5804° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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