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 57751U 26145.53700922 +.00000000 +00000-0 +64444-3 0 00009
2 57751 43.0000 82.7759 0001899 205.2612 154.8148 15.30094088 06
| Epoch (UTC): | 25 May 2026 12:53:17 |
| Eccentricity: | 0.0001899 |
| inclination: | 43.0000° |
| perigee height: | 474 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 82.7759° |
| argument of perigee: | 205.2612° |
| revolutions per day: | 15.30094088 |
| mean anomaly at epoch: | 154.8148° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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