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 67918U 26145.42995756 +.00000000 +00000-0 +51475-3 0 00004
2 67918 42.9985 172.3114 0001667 271.1616 88.9045 15.27593510 05
| Epoch (UTC): | 25 May 2026 10:19:08 |
| Eccentricity: | 0.0001667 |
| inclination: | 42.9985° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 172.3114° |
| argument of perigee: | 271.1616° |
| revolutions per day: | 15.27593510 |
| mean anomaly at epoch: | 88.9045° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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