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 68835U 26145.58748427 +.00000000 +00000-0 +15821-3 0 00006
2 68835 38.0001 222.9367 0004796 218.3973 141.6448 15.06552928 05
| Epoch (UTC): | 25 May 2026 14:05:58 |
| Eccentricity: | 0.0004796 |
| inclination: | 38.0001° |
| perigee height: | 543 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 222.9367° |
| argument of perigee: | 218.3973° |
| revolutions per day: | 15.06552928 |
| mean anomaly at epoch: | 141.6448° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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