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 12786U 26020.97393650 +.00000000 +00000-0 +86041-4 0 00002
2 12786 82.4856 245.7539 0015977 326.1675 33.8522 14.87078296 08
| Epoch (UTC): | 20 January 2026 23:22:28 |
| Eccentricity: | 0.0015977 |
| inclination: | 82.4856° |
| perigee height: | 596 km |
| apogee height: | 618 km |
| right ascension of ascending node: | 245.7539° |
| argument of perigee: | 326.1675° |
| revolutions per day: | 14.87078296 |
| mean anomaly at epoch: | 33.8522° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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