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 67924U 26145.53887812 +.00000000 +00000-0 +49538-3 0 00003
2 67924 43.0004 171.3897 0001478 270.8237 89.2445 15.27601308 01
| Epoch (UTC): | 25 May 2026 12:55:59 |
| Eccentricity: | 0.0001478 |
| inclination: | 43.0004° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 171.3897° |
| argument of perigee: | 270.8237° |
| revolutions per day: | 15.27601308 |
| mean anomaly at epoch: | 89.2445° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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