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 40976U 26145.09403757 +.00000000 +00000-0 +26832-3 0 00006
2 40976 64.7761 6.8014 0129954 69.9714 291.5333 14.89072710 09
| Epoch (UTC): | 25 May 2026 02:15:24 |
| Eccentricity: | 0.0129954 |
| inclination: | 64.7761° |
| perigee height: | 510 km |
| apogee height: | 692 km |
| right ascension of ascending node: | 6.8014° |
| argument of perigee: | 69.9714° |
| revolutions per day: | 14.89072710 |
| mean anomaly at epoch: | 291.5333° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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