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 68332U 26145.30795862 +.00000000 +00000-0 +28999-3 0 00003
2 68332 53.1604 352.5739 0001482 84.0790 276.0379 15.30218241 01
| Epoch (UTC): | 25 May 2026 07:23:27 |
| Eccentricity: | 0.0001482 |
| inclination: | 53.1604° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 352.5739° |
| argument of perigee: | 84.0790° |
| revolutions per day: | 15.30218241 |
| mean anomaly at epoch: | 276.0379° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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