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 12667U 26104.65412954 +.00000000 +00000-0 +40000-3 0 00001
2 12667 82.8364 66.2700 0032091 249.3678 289.6040 13.83565932 04
| Epoch (UTC): | 14 April 2026 15:41:56 |
| Eccentricity: | 0.0032091 |
| inclination: | 82.8364° |
| perigee height: | 928 km |
| apogee height: | 975 km |
| right ascension of ascending node: | 66.2700° |
| argument of perigee: | 249.3678° |
| revolutions per day: | 13.83565932 |
| mean anomaly at epoch: | 289.6040° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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