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 47648U 26145.12821944 +.00000000 +00000-0 +84626-4 0 00001
2 47648 53.1612 54.0117 0001241 95.8187 264.2955 15.31709414 01
| Epoch (UTC): | 25 May 2026 03:04:38 |
| Eccentricity: | 0.0001241 |
| inclination: | 53.1612° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 54.0117° |
| argument of perigee: | 95.8187° |
| revolutions per day: | 15.31709414 |
| mean anomaly at epoch: | 264.2955° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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