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 40967U 26100.79904220 +.00000000 +00000-0 +20677-3 0 00006
2 40967 64.7741 128.3375 0128346 83.0442 278.5249 14.90572180 05
| Epoch (UTC): | 10 April 2026 19:10:37 |
| Eccentricity: | 0.0128346 |
| inclination: | 64.7741° |
| perigee height: | 507 km |
| apogee height: | 686 km |
| right ascension of ascending node: | 128.3375° |
| argument of perigee: | 83.0442° |
| revolutions per day: | 14.90572180 |
| mean anomaly at epoch: | 278.5249° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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