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 26160.11731531 +.00000000 +00000-0 +39509-4 0 00004
2 12786 82.4871 114.0986 0015711 216.3450 143.6702 14.87216224 01
| Epoch (UTC): | 09 June 2026 02:48:56 |
| Eccentricity: | 0.0015711 |
| inclination: | 82.4871° |
| perigee height: | 596 km |
| apogee height: | 618 km |
| right ascension of ascending node: | 114.0986° |
| argument of perigee: | 216.3450° |
| revolutions per day: | 14.87216224 |
| mean anomaly at epoch: | 143.6702° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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