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 56692U 26145.21117522 +.00000000 +00000-0 +42243-4 0 00009
2 56692 43.0027 209.0736 0001500 269.9685 90.0995 15.27578420 07
| Epoch (UTC): | 25 May 2026 05:04:05 |
| Eccentricity: | 0.0001500 |
| inclination: | 43.0027° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 209.0736° |
| argument of perigee: | 269.9685° |
| revolutions per day: | 15.27578420 |
| mean anomaly at epoch: | 90.0995° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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