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 68393U 26145.34390044 +.00000000 +00000-0 +94208-3 0 00003
2 68393 97.2842 287.9168 0001524 90.0906 270.0511 15.33462062 08
| Epoch (UTC): | 25 May 2026 08:15:12 |
| Eccentricity: | 0.0001524 |
| inclination: | 97.2842° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 287.9168° |
| argument of perigee: | 90.0906° |
| revolutions per day: | 15.33462062 |
| mean anomaly at epoch: | 270.0511° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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