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 67316U 26145.59422715 +.00000000 +00000-0 +66483-3 0 00009
2 67316 43.0001 250.6743 0001072 284.2682 75.8051 15.27597884 04
| Epoch (UTC): | 25 May 2026 14:15:41 |
| Eccentricity: | 0.0001072 |
| inclination: | 43.0001° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 250.6743° |
| argument of perigee: | 284.2682° |
| revolutions per day: | 15.27597884 |
| mean anomaly at epoch: | 75.8051° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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