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 68431U 26144.86110743 +.00000000 +00000-0 +31998-3 0 00005
2 68431 97.4588 103.7383 0004373 82.7637 277.4095 15.18659766 08
| Epoch (UTC): | 24 May 2026 20:39:59 |
| Eccentricity: | 0.0004373 |
| inclination: | 97.4588° |
| perigee height: | 507 km |
| apogee height: | 513 km |
| right ascension of ascending node: | 103.7383° |
| argument of perigee: | 82.7637° |
| revolutions per day: | 15.18659766 |
| mean anomaly at epoch: | 277.4095° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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