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 68428U 26145.39553093 +.00000000 +00000-0 +17432-3 0 00006
2 68428 97.4559 104.2265 0003563 83.2467 276.9173 15.18301440 08
| Epoch (UTC): | 25 May 2026 09:29:33 |
| Eccentricity: | 0.0003563 |
| inclination: | 97.4559° |
| perigee height: | 509 km |
| apogee height: | 513 km |
| right ascension of ascending node: | 104.2265° |
| argument of perigee: | 83.2467° |
| revolutions per day: | 15.18301440 |
| mean anomaly at epoch: | 276.9173° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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