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 67318U 26145.55840230 +.00000000 +00000-0 +90056-3 0 00006
2 67318 43.0032 251.2713 0001571 268.7705 91.2966 15.27624449 06
| Epoch (UTC): | 25 May 2026 13:24:05 |
| Eccentricity: | 0.0001571 |
| inclination: | 43.0032° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 251.2713° |
| argument of perigee: | 268.7705° |
| revolutions per day: | 15.27624449 |
| mean anomaly at epoch: | 91.2966° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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