Kosmos 145 was the second of two DS-U2-M satellites to be launched, after Kosmos 97.[3][6] It was operated in an orbit with a perigee of 215 kilometres (134 mi), an apogee of 2,116 kilometres (1,315 mi), an inclination of 48.4°, and an orbital period of 108.6 minutes.[2] On 8 March 1968, it decayed from orbit and reentered the atmosphere.[7]
Payloads are separated by bullets ( · ), launches by pipes ( | ). Crewed flights are indicated in underline. Uncatalogued launch failures are listed in italics. Payloads deployed from other spacecraft are denoted in (brackets).
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