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 20776U 26150.15330417 +.00000000 +00000-0 +00000-0 0 00003
2 20776 13.3456 349.9408 0002935 74.7366 271.5858 1.00269291 01
| Epoch (UTC): | 30 May 2026 03:40:45 |
| Eccentricity: | 0.0002935 |
| inclination: | 13.3456° |
| perigee height: | 35775 km |
| apogee height: | 35800 km |
| right ascension of ascending node: | 349.9408° |
| argument of perigee: | 74.7366° |
| revolutions per day: | 1.00269291 |
| mean anomaly at epoch: | 271.5858° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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