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 47356U 26145.41349375 +.00000000 +00000-0 -43975-4 0 00005
2 47356 53.1602 40.1249 0001304 76.2142 283.9005 15.31697199 02
| Epoch (UTC): | 25 May 2026 09:55:25 |
| Eccentricity: | 0.0001304 |
| inclination: | 53.1602° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 40.1249° |
| argument of perigee: | 76.2142° |
| revolutions per day: | 15.31697199 |
| mean anomaly at epoch: | 283.9005° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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