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 26073.69211595 +.00000000 +00000-0 +42003-3 0 00007
2 40967 64.7751 212.5104 0128748 93.9133 267.6709 14.90402302 03
| Epoch (UTC): | 14 March 2026 16:36:38 |
| Eccentricity: | 0.0128748 |
| inclination: | 64.7751° |
| perigee height: | 507 km |
| apogee height: | 686 km |
| right ascension of ascending node: | 212.5104° |
| argument of perigee: | 93.9133° |
| revolutions per day: | 14.90402302 |
| mean anomaly at epoch: | 267.6709° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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