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 26103.12924847 +.00000000 +00000-0 +26811-4 0 00008
2 12786 82.4894 168.0272 0017960 53.0121 307.2736 14.87178118 06
| Epoch (UTC): | 13 April 2026 03:06:07 |
| Eccentricity: | 0.0017960 |
| inclination: | 82.4894° |
| perigee height: | 594 km |
| apogee height: | 619 km |
| right ascension of ascending node: | 168.0272° |
| argument of perigee: | 53.0121° |
| revolutions per day: | 14.87178118 |
| mean anomaly at epoch: | 307.2736° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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