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 47630U 26145.17015117 +.00000000 +00000-0 +21949-3 0 00002
2 47630 53.1594 53.8598 0001099 88.2398 271.8729 15.31738868 00
| Epoch (UTC): | 25 May 2026 04:05:01 |
| Eccentricity: | 0.0001099 |
| inclination: | 53.1594° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 53.8598° |
| argument of perigee: | 88.2398° |
| revolutions per day: | 15.31738868 |
| mean anomaly at epoch: | 271.8729° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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