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 47389U 26145.12915196 +.00000000 +00000-0 +16424-3 0 00006
2 47389 53.1599 41.2174 0001246 95.2358 264.8785 15.31715615 04
| Epoch (UTC): | 25 May 2026 03:05:58 |
| Eccentricity: | 0.0001246 |
| inclination: | 53.1599° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 41.2174° |
| argument of perigee: | 95.2358° |
| revolutions per day: | 15.31715615 |
| mean anomaly at epoch: | 264.8785° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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