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 12456U 26100.19487949 +.00000000 +00000-0 +61309-4 0 00004
2 12456 81.2672 165.2149 0046323 324.7424 35.0685 14.11042066 00
| Epoch (UTC): | 10 April 2026 04:40:37 |
| Eccentricity: | 0.0046323 |
| inclination: | 81.2672° |
| perigee height: | 822 km |
| apogee height: | 889 km |
| right ascension of ascending node: | 165.2149° |
| argument of perigee: | 324.7424° |
| revolutions per day: | 14.11042066 |
| mean anomaly at epoch: | 35.0685° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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