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 67403U 26145.52709845 +.00000000 +00000-0 +00000-0 0 00001
2 67403 3.3413 95.6455 0007636 351.7743 59.3653 1.00273714 08
| Epoch (UTC): | 25 May 2026 12:39:01 |
| Eccentricity: | 0.0007636 |
| inclination: | 3.3413° |
| perigee height: | 35754 km |
| apogee height: | 35818 km |
| right ascension of ascending node: | 95.6455° |
| argument of perigee: | 351.7743° |
| revolutions per day: | 1.00273714 |
| mean anomaly at epoch: | 59.3653° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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