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 68341U 26144.59729426 +.00000000 +00000-0 +81677-3 0 00008
2 68341 53.1588 351.6695 0002954 93.0619 267.0721 15.34429703 00
| Epoch (UTC): | 24 May 2026 14:20:06 |
| Eccentricity: | 0.0002954 |
| inclination: | 53.1588° |
| perigee height: | 461 km |
| apogee height: | 465 km |
| right ascension of ascending node: | 351.6695° |
| argument of perigee: | 93.0619° |
| revolutions per day: | 15.34429703 |
| mean anomaly at epoch: | 267.0721° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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