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 67308U 26145.02632781 +.00000000 +00000-0 +68164-3 0 00002
2 67308 43.0045 254.1568 0001893 278.5094 81.5543 15.27573235 05
| Epoch (UTC): | 25 May 2026 00:37:54 |
| Eccentricity: | 0.0001893 |
| inclination: | 43.0045° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 254.1568° |
| argument of perigee: | 278.5094° |
| revolutions per day: | 15.27573235 |
| mean anomaly at epoch: | 81.5543° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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