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 68532U 26145.26546140 +.00000000 +00000-0 +63407-3 0 00006
2 68532 53.1588 132.5430 0001703 58.7047 301.4122 15.34412582 04
| Epoch (UTC): | 25 May 2026 06:22:15 |
| Eccentricity: | 0.0001703 |
| inclination: | 53.1588° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 132.5430° |
| argument of perigee: | 58.7047° |
| revolutions per day: | 15.34412582 |
| mean anomaly at epoch: | 301.4122° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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