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 68264U 26145.58335647 +.00000000 +00000-0 -33170-4 0 00007
2 68264 53.1602 321.0149 0001203 94.0268 102.2842 15.34395714 01
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001203 |
| inclination: | 53.1602° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 321.0149° |
| argument of perigee: | 94.0268° |
| revolutions per day: | 15.34395714 |
| mean anomaly at epoch: | 102.2842° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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