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 67674U 26145.46758373 +.00000000 +00000-0 +12662-3 0 00004
2 67674 96.6530 218.6005 0010755 177.2457 182.8875 15.82801257 02
| Epoch (UTC): | 25 May 2026 11:13:19 |
| Eccentricity: | 0.0010755 |
| inclination: | 96.6530° |
| perigee height: | 315 km |
| apogee height: | 330 km |
| right ascension of ascending node: | 218.6005° |
| argument of perigee: | 177.2457° |
| revolutions per day: | 15.82801257 |
| mean anomaly at epoch: | 182.8875° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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