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 12769U 26108.50327397 +.00000000 +00000-0 +55035-3 0 00002
2 12769 82.8239 188.7002 0071561 174.2637 205.9585 13.74041296 06
| Epoch (UTC): | 18 April 2026 12:04:42 |
| Eccentricity: | 0.0071561 |
| inclination: | 82.8239° |
| perigee height: | 932 km |
| apogee height: | 1038 km |
| right ascension of ascending node: | 188.7002° |
| argument of perigee: | 174.2637° |
| revolutions per day: | 13.74041296 |
| mean anomaly at epoch: | 205.9585° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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