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 47401U 26145.11519691 +.00000000 +00000-0 +38427-4 0 00008
2 47401 53.1612 41.5018 0001199 83.6414 276.4723 15.31716667 05
| Epoch (UTC): | 25 May 2026 02:45:53 |
| Eccentricity: | 0.0001199 |
| inclination: | 53.1612° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 41.5018° |
| argument of perigee: | 83.6414° |
| revolutions per day: | 15.31716667 |
| mean anomaly at epoch: | 276.4723° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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