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 56127U 26145.53264782 +.00000000 +00000-0 -44862-4 0 00008
2 56127 43.0024 76.3198 0000900 259.3485 100.7266 15.27561277 00
| Epoch (UTC): | 25 May 2026 12:47:00 |
| Eccentricity: | 0.0000900 |
| inclination: | 43.0024° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 76.3198° |
| argument of perigee: | 259.3485° |
| revolutions per day: | 15.27561277 |
| mean anomaly at epoch: | 100.7266° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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