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 00011U 26088.18583329 +.00000000 +00000-0 +82847-3 0 00000
2 00011 32.8751 27.9083 1445178 321.5863 28.9975 11.90307438 03
| Epoch (UTC): | 29 March 2026 04:27:35 |
| Eccentricity: | 0.1445178 |
| inclination: | 32.8751° |
| perigee height: | 554 km |
| apogee height: | 2896 km |
| right ascension of ascending node: | 27.9083° |
| argument of perigee: | 321.5863° |
| revolutions per day: | 11.90307438 |
| mean anomaly at epoch: | 28.9975° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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