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 47122U 26145.36952227 +.00000000 +00000-0 +68184-3 0 00003
2 47122 53.0465 270.5072 0003773 243.4408 116.6220 15.66005324 09
| Epoch (UTC): | 25 May 2026 08:52:06 |
| Eccentricity: | 0.0003773 |
| inclination: | 53.0465° |
| perigee height: | 368 km |
| apogee height: | 373 km |
| right ascension of ascending node: | 270.5072° |
| argument of perigee: | 243.4408° |
| revolutions per day: | 15.66005324 |
| mean anomaly at epoch: | 116.6220° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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