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 68446U 26144.83060034 +.00000000 +00000-0 +81764-3 0 00001
2 68446 97.4390 103.4941 0008557 140.1456 220.0407 15.18147324 01
| Epoch (UTC): | 24 May 2026 19:56:03 |
| Eccentricity: | 0.0008557 |
| inclination: | 97.4390° |
| perigee height: | 506 km |
| apogee height: | 517 km |
| right ascension of ascending node: | 103.4941° |
| argument of perigee: | 140.1456° |
| revolutions per day: | 15.18147324 |
| mean anomaly at epoch: | 220.0407° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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