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 57511U 26145.42632990 +.00000000 +00000-0 +10632-3 0 00000
2 57511 43.0040 302.4849 0002570 265.6506 94.4052 15.27581471 01
| Epoch (UTC): | 25 May 2026 10:13:54 |
| Eccentricity: | 0.0002570 |
| inclination: | 43.0040° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 302.4849° |
| argument of perigee: | 265.6506° |
| revolutions per day: | 15.27581471 |
| mean anomaly at epoch: | 94.4052° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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