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 26069.80025514 +.00000000 +00000-0 +40787-3 0 00006
2 40967 64.7749 224.5937 0128853 95.4595 266.1231 14.90367024 08
| Epoch (UTC): | 10 March 2026 19:12:22 |
| Eccentricity: | 0.0128853 |
| inclination: | 64.7749° |
| perigee height: | 507 km |
| apogee height: | 687 km |
| right ascension of ascending node: | 224.5937° |
| argument of perigee: | 95.4595° |
| revolutions per day: | 14.90367024 |
| mean anomaly at epoch: | 266.1231° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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