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 62037U 26145.59173688 +.00000000 +00000-0 +52922-3 0 00009
2 62037 43.0008 189.2155 0001930 276.6163 83.4469 15.27593205 03
| Epoch (UTC): | 25 May 2026 14:12:06 |
| Eccentricity: | 0.0001930 |
| inclination: | 43.0008° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 189.2155° |
| argument of perigee: | 276.6163° |
| revolutions per day: | 15.27593205 |
| mean anomaly at epoch: | 83.4469° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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