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 00167U 26098.72133321 +.00000000 +00000-0 +60418-4 0 00007
2 00167 47.8473 353.5132 0090087 187.4930 172.4612 14.24142098 05
| Epoch (UTC): | 08 April 2026 17:18:43 |
| Eccentricity: | 0.0090087 |
| inclination: | 47.8473° |
| perigee height: | 747 km |
| apogee height: | 876 km |
| right ascension of ascending node: | 353.5132° |
| argument of perigee: | 187.4930° |
| revolutions per day: | 14.24142098 |
| mean anomaly at epoch: | 172.4612° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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