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 65786U 26145.47549375 +.00000000 +00000-0 +31105-3 0 00000
2 65786 51.9011 53.5629 0001204 75.4222 284.6873 14.79940180 01
| Epoch (UTC): | 25 May 2026 11:24:42 |
| Eccentricity: | 0.0001204 |
| inclination: | 51.9011° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 53.5629° |
| argument of perigee: | 75.4222° |
| revolutions per day: | 14.79940180 |
| mean anomaly at epoch: | 284.6873° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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