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 40972U 26145.57899838 +.00000000 +00000-0 +10842-2 0 00007
2 40972 64.7432 172.6594 0033606 27.2167 333.0729 15.56105970 03
| Epoch (UTC): | 25 May 2026 13:53:45 |
| Eccentricity: | 0.0033606 |
| inclination: | 64.7432° |
| perigee height: | 376 km |
| apogee height: | 422 km |
| right ascension of ascending node: | 172.6594° |
| argument of perigee: | 27.2167° |
| revolutions per day: | 15.56105970 |
| mean anomaly at epoch: | 333.0729° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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