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 34661U 26143.23442146 +.00000000 +00000-0 +00000-0 0 00005
2 34661 54.4863 211.6557 0144216 61.5748 18.4350 2.00553310 08
| Epoch (UTC): | 23 May 2026 05:37:34 |
| Eccentricity: | 0.0144216 |
| inclination: | 54.4863° |
| perigee height: | 19800 km |
| apogee height: | 20566 km |
| right ascension of ascending node: | 211.6557° |
| argument of perigee: | 61.5748° |
| revolutions per day: | 2.00553310 |
| mean anomaly at epoch: | 18.4350° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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