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 26145.18254271 +.00000000 +00000-0 +00000-0 0 00003
2 20776 13.3469 349.9765 0002773 60.3170 291.5741 1.00276402 00
| Epoch (UTC): | 25 May 2026 04:22:51 |
| Eccentricity: | 0.0002773 |
| inclination: | 13.3469° |
| perigee height: | 35774 km |
| apogee height: | 35797 km |
| right ascension of ascending node: | 349.9765° |
| argument of perigee: | 60.3170° |
| revolutions per day: | 1.00276402 |
| mean anomaly at epoch: | 291.5741° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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