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 59776U 26145.29986306 +.00000000 +00000-0 +54754-3 0 00006
2 59776 97.6541 277.4503 0006822 222.8585 137.2127 15.36009001 04
| Epoch (UTC): | 25 May 2026 07:11:48 |
| Eccentricity: | 0.0006822 |
| inclination: | 97.6541° |
| perigee height: | 453 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 277.4503° |
| argument of perigee: | 222.8585° |
| revolutions per day: | 15.36009001 |
| mean anomaly at epoch: | 137.2127° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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