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 26145.54620242 +.00000000 +00000-0 +27967-3 0 00006
2 40967 64.7765 349.3386 0129440 65.4886 295.9658 14.90820633 06
| Epoch (UTC): | 25 May 2026 13:06:31 |
| Eccentricity: | 0.0129440 |
| inclination: | 64.7765° |
| perigee height: | 505 km |
| apogee height: | 686 km |
| right ascension of ascending node: | 349.3386° |
| argument of perigee: | 65.4886° |
| revolutions per day: | 14.90820633 |
| mean anomaly at epoch: | 295.9658° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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