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 62773U 26145.58335647 +.00000000 +00000-0 -13265-4 0 00009
2 62773 53.1604 325.0036 0001015 86.6890 68.6890 15.34396062 05
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001015 |
| inclination: | 53.1604° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 325.0036° |
| argument of perigee: | 86.6890° |
| revolutions per day: | 15.34396062 |
| mean anomaly at epoch: | 68.6890° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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