The invention belongs to the technical field of special glass, and provides anti-ultraviolet absorption space radiation-resistant glass which comprises the following raw materials in parts by mass: 1.2-5.9 parts of cerium dioxide, 0.5-4.6 parts of neodymium oxide, 0.8-3.2 parts of lanthanum oxide, 0.7-3.5 parts of ytterbium oxide, 3.4-12.3 parts of sodium carbonate, 0.4-4.7 parts of aluminum oxide, 72.2-78.3 parts of silica sand, 5.7-10.7 parts of strontium carbonate, 4.6-11.3 parts of BaCO3, 0.3-1.5 parts of SeO2, 0.9-2.5 parts of bismuth trioxide, 0.5-1.6 parts of tellurium dioxide, 4.8-10 parts of potassium nitrate, 1.2-2.5 parts of antimonous oxide and 0.7-1.6 parts of sodium pyroantimonate. According to the technical scheme, the problem that in the prior art, the anti-irradiation performance, transmittance and mechanical strength of common glass in space application cannot meet deep space exploration is solved.