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 40012U 26053.67334880 +.00000000 +00000-0 +40391-3 0 00005
2 40012 97.7701 208.5601 0046739 86.2899 274.3660 14.87508675 02
| Epoch (UTC): | 22 February 2026 16:09:37 |
| Eccentricity: | 0.0046739 |
| inclination: | 97.7701° |
| perigee height: | 573 km |
| apogee height: | 638 km |
| right ascension of ascending node: | 208.5601° |
| argument of perigee: | 86.2899° |
| revolutions per day: | 14.87508675 |
| mean anomaly at epoch: | 274.3660° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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