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 12586U 26018.64932387 +.00000000 +00000-0 +23293-3 0 00006
2 12586 97.6419 59.2886 0012148 172.2502 187.8929 15.32303870 09
| Epoch (UTC): | 18 January 2026 15:35:01 |
| Eccentricity: | 0.0012148 |
| inclination: | 97.6419° |
| perigee height: | 461 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 59.2886° |
| argument of perigee: | 172.2502° |
| revolutions per day: | 15.32303870 |
| mean anomaly at epoch: | 187.8929° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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