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 68864U 26145.58335647 +.00000000 +00000-0 -54768-1 0 00006
2 68864 51.8807 352.4853 0009081 224.9939 2.2101 15.21633845 03
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0009081 |
| inclination: | 51.8807° |
| perigee height: | 495 km |
| apogee height: | 507 km |
| right ascension of ascending node: | 352.4853° |
| argument of perigee: | 224.9939° |
| revolutions per day: | 15.21633845 |
| mean anomaly at epoch: | 2.2101° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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