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 47691U 26145.57130041 +.00000000 +00000-0 +63568-4 0 00001
2 47691 63.4039 255.9703 0175068 0.5886 359.5315 13.45447949 00
| Epoch (UTC): | 25 May 2026 13:42:40 |
| Eccentricity: | 0.0175068 |
| inclination: | 63.4039° |
| perigee height: | 958 km |
| apogee height: | 1220 km |
| right ascension of ascending node: | 255.9703° |
| argument of perigee: | 0.5886° |
| revolutions per day: | 13.45447949 |
| mean anomaly at epoch: | 359.5315° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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