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 67109U 26145.55735078 +.00000000 +00000-0 +37104-3 0 00002
2 67109 43.0004 94.7545 0000593 244.8194 115.2596 15.27593077 04
| Epoch (UTC): | 25 May 2026 13:22:35 |
| Eccentricity: | 0.0000593 |
| inclination: | 43.0004° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 94.7545° |
| argument of perigee: | 244.8194° |
| revolutions per day: | 15.27593077 |
| mean anomaly at epoch: | 115.2596° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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