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 59520U 26145.32470053 +.00000000 +00000-0 +18745-5 0 00006
2 59520 43.0017 245.4247 0001559 272.2545 87.8128 15.27574527 02
| Epoch (UTC): | 25 May 2026 07:47:34 |
| Eccentricity: | 0.0001559 |
| inclination: | 43.0017° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 245.4247° |
| argument of perigee: | 272.2545° |
| revolutions per day: | 15.27574527 |
| mean anomaly at epoch: | 87.8128° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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