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 67908U 26145.47991759 +.00000000 +00000-0 +72345-3 0 00006
2 67908 43.0004 171.8117 0001769 270.9742 89.0907 15.27607044 02
| Epoch (UTC): | 25 May 2026 11:31:04 |
| Eccentricity: | 0.0001769 |
| inclination: | 43.0004° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 171.8117° |
| argument of perigee: | 270.9742° |
| revolutions per day: | 15.27607044 |
| mean anomaly at epoch: | 89.0907° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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