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 67149U 26145.26082755 +.00000000 +00000-0 +46451-3 0 00006
2 67149 51.9022 97.0356 0000800 83.3627 276.7426 14.79944159 02
| Epoch (UTC): | 25 May 2026 06:15:35 |
| Eccentricity: | 0.0000800 |
| inclination: | 51.9022° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 97.0356° |
| argument of perigee: | 83.3627° |
| revolutions per day: | 14.79944159 |
| mean anomaly at epoch: | 276.7426° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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