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 62832U 26145.53306080 +.00000000 +00000-0 +20735-2 0 00006
2 62832 43.0004 203.0265 0001239 266.1965 93.8761 15.70888869 06
| Epoch (UTC): | 25 May 2026 12:47:36 |
| Eccentricity: | 0.0001239 |
| inclination: | 43.0004° |
| perigee height: | 356 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 203.0265° |
| argument of perigee: | 266.1965° |
| revolutions per day: | 15.70888869 |
| mean anomaly at epoch: | 93.8761° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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