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 26020.71350187 +.00000000 +00000-0 +98545-3 0 00006
2 34712 46.0013 21.1635 4922876 115.6239 302.6036 5.68484222 07
| Epoch (UTC): | 20 January 2026 17:07:26 |
| Eccentricity: | 0.4922876 |
| inclination: | 46.0013° |
| perigee height: | 355 km |
| apogee height: | 13412 km |
| right ascension of ascending node: | 21.1635° |
| argument of perigee: | 115.6239° |
| revolutions per day: | 5.68484222 |
| mean anomaly at epoch: | 302.6036° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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