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 67569U 26145.44414965 +.00000000 +00000-0 +80940-3 0 00005
2 67569 97.2853 206.7847 0000191 145.4721 214.6535 15.33452837 05
| Epoch (UTC): | 25 May 2026 10:39:34 |
| Eccentricity: | 0.0000191 |
| inclination: | 97.2853° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 206.7847° |
| argument of perigee: | 145.4721° |
| revolutions per day: | 15.33452837 |
| mean anomaly at epoch: | 214.6535° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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