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 64920U 26144.99763397 +.00000000 +00000-0 +10225-2 0 00006
2 64920 53.1589 351.4550 0001053 77.6384 282.4734 15.30189634 01
| Epoch (UTC): | 24 May 2026 23:56:35 |
| Eccentricity: | 0.0001053 |
| inclination: | 53.1589° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 351.4550° |
| argument of perigee: | 77.6384° |
| revolutions per day: | 15.30189634 |
| mean anomaly at epoch: | 282.4734° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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