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 67113U 26145.25356707 +.00000000 +00000-0 +14500-2 0 00006
2 67113 43.0032 96.7772 0001782 250.9185 109.1474 15.27601753 01
| Epoch (UTC): | 25 May 2026 06:05:08 |
| Eccentricity: | 0.0001782 |
| inclination: | 43.0032° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 96.7772° |
| argument of perigee: | 250.9185° |
| revolutions per day: | 15.27601753 |
| mean anomaly at epoch: | 109.1474° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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