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 68859U 26145.50003470 +.00000000 +00000-0 +17318-2 0 00008
2 68859 97.2852 160.2421 0000768 112.0746 122.3387 15.49138282 08
| Epoch (UTC): | 25 May 2026 12:00:02 |
| Eccentricity: | 0.0000768 |
| inclination: | 97.2852° |
| perigee height: | 419 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 160.2421° |
| argument of perigee: | 112.0746° |
| revolutions per day: | 15.49138282 |
| mean anomaly at epoch: | 122.3387° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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