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 26071.61199464 +.00000000 +00000-0 +39273-3 0 00002
2 40967 64.7750 218.9685 0128813 94.7295 266.8541 14.90383322 02
| Epoch (UTC): | 12 March 2026 14:41:16 |
| Eccentricity: | 0.0128813 |
| inclination: | 64.7750° |
| perigee height: | 507 km |
| apogee height: | 687 km |
| right ascension of ascending node: | 218.9685° |
| argument of perigee: | 94.7295° |
| revolutions per day: | 14.90383322 |
| mean anomaly at epoch: | 266.8541° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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