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 59778U 26145.62559189 +.00000000 +00000-0 +52066-3 0 00004
2 59778 97.6540 278.0485 0007172 221.3479 138.7223 15.36644569 03
| Epoch (UTC): | 25 May 2026 15:00:51 |
| Eccentricity: | 0.0007172 |
| inclination: | 97.6540° |
| perigee height: | 451 km |
| apogee height: | 461 km |
| right ascension of ascending node: | 278.0485° |
| argument of perigee: | 221.3479° |
| revolutions per day: | 15.36644569 |
| mean anomaly at epoch: | 138.7223° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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