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 67949U 26145.63661102 +.00000000 +00000-0 +26014-3 0 00007
2 67949 43.0015 115.7362 0001737 275.5077 84.5577 15.27582994 04
| Epoch (UTC): | 25 May 2026 15:16:43 |
| Eccentricity: | 0.0001737 |
| inclination: | 43.0015° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 115.7362° |
| argument of perigee: | 275.5077° |
| revolutions per day: | 15.27582994 |
| mean anomaly at epoch: | 84.5577° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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