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 67677U 26145.62456006 +.00000000 +00000-0 +33032-3 0 00007
2 67677 96.6330 209.7584 0018045 210.5262 149.4929 15.24327212 00
| Epoch (UTC): | 25 May 2026 14:59:21 |
| Eccentricity: | 0.0018045 |
| inclination: | 96.6330° |
| perigee height: | 480 km |
| apogee height: | 505 km |
| right ascension of ascending node: | 209.7584° |
| argument of perigee: | 210.5262° |
| revolutions per day: | 15.24327212 |
| mean anomaly at epoch: | 149.4929° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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