Kosmos 803 was placed into a low Earth orbit with a perigee of 505 kilometres (314 mi), an apogee of 555 kilometres (345 mi), 65.9 degrees of inclination, and an orbital period of 95.2 minutes.[1] It was used for a non-destructive intercept test, with both Kosmos 804 and Kosmos 814 intercepting it before deorbiting themselves. As of 2009, it is still in orbit.[2][5]
Kosmos 803 was the second of ten Lira satellites to be launched,[1] of which all but the first were successful. It was the first Lira satellite to successfully reach orbit. Lira was derived from the earlier DS-P1-M satellite, which it replaced.
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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