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 34712U 26063.94738505 +.00000000 +00000-0 +88910-3 0 00007
2 34712 45.9977 340.8511 4921073 156.5912 236.9951 5.68661765 02
| Epoch (UTC): | 04 March 2026 22:44:14 |
| Eccentricity: | 0.4921073 |
| inclination: | 45.9977° |
| perigee height: | 356 km |
| apogee height: | 13405 km |
| right ascension of ascending node: | 340.8511° |
| argument of perigee: | 156.5912° |
| revolutions per day: | 5.68661765 |
| mean anomaly at epoch: | 236.9951° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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