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 55617U 26145.39570190 +.00000000 +00000-0 +31720-4 0 00006
2 55617 43.0059 280.7576 0001800 274.3120 85.7526 15.27581540 01
| Epoch (UTC): | 25 May 2026 09:29:48 |
| Eccentricity: | 0.0001800 |
| inclination: | 43.0059° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 280.7576° |
| argument of perigee: | 274.3120° |
| revolutions per day: | 15.27581540 |
| mean anomaly at epoch: | 85.7526° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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