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 68011U 26145.56843462 +.00000000 +00000-0 +81481-3 0 00000
2 68011 43.0028 334.5464 0001373 278.1191 81.9505 15.27594767 08
| Epoch (UTC): | 25 May 2026 13:38:32 |
| Eccentricity: | 0.0001373 |
| inclination: | 43.0028° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 334.5464° |
| argument of perigee: | 278.1191° |
| revolutions per day: | 15.27594767 |
| mean anomaly at epoch: | 81.9505° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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