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 68558U 26145.58335647 +.00000000 +00000-0 +13141-2 0 00006
2 68558 53.1589 4.8133 0001051 115.7027 331.4359 15.34370696 06
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001051 |
| inclination: | 53.1589° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 4.8133° |
| argument of perigee: | 115.7027° |
| revolutions per day: | 15.34370696 |
| mean anomaly at epoch: | 331.4359° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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