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 68233U 26145.44918179 +.00000000 +00000-0 +11971-2 0 00007
2 68233 53.1580 296.1029 0003069 77.2855 282.8497 15.49367602 00
| Epoch (UTC): | 25 May 2026 10:46:49 |
| Eccentricity: | 0.0003069 |
| inclination: | 53.1580° |
| perigee height: | 416 km |
| apogee height: | 421 km |
| right ascension of ascending node: | 296.1029° |
| argument of perigee: | 77.2855° |
| revolutions per day: | 15.49367602 |
| mean anomaly at epoch: | 282.8497° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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