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 26072.81981035 +.00000000 +00000-0 +37386-3 0 00001
2 40967 64.7749 215.2186 0128775 94.2556 267.3284 14.90393335 03
| Epoch (UTC): | 13 March 2026 19:40:31 |
| Eccentricity: | 0.0128775 |
| inclination: | 64.7749° |
| perigee height: | 507 km |
| apogee height: | 687 km |
| right ascension of ascending node: | 215.2186° |
| argument of perigee: | 94.2556° |
| revolutions per day: | 14.90393335 |
| mean anomaly at epoch: | 267.3284° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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