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 67642U 26145.47769297 +.00000000 +00000-0 +59950-3 0 00008
2 67642 42.9959 66.4319 0001222 265.0588 95.0124 15.27589329 07
| Epoch (UTC): | 25 May 2026 11:27:52 |
| Eccentricity: | 0.0001222 |
| inclination: | 42.9959° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 66.4319° |
| argument of perigee: | 265.0588° |
| revolutions per day: | 15.27589329 |
| mean anomaly at epoch: | 95.0124° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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