The development of spacecraft for electronic surveillance of radar systems was split into two phases:
Phase 1 included development of electronic surveillance spacecraft, based on experience in developing the unified DS-U1 and DS-U2 spacecraft, and launch of two experimental DS-K 40 spacecraft. Both launches were unsuccessful due to launch vehicle failure. Phase 2 included development of electronic surveillance spacecraft for the Tselina system. The spacecraft incorporated much lighter payload instrumentation based on microcomponents.
The Tselina-О, Tselina-D, Tselina-2, and Tselina-R spacecraft met all objectives of electronic surveillance.

Tselina-О
|
Mass, kg |
339…434 |
| Active life, months | 6 |
| Launch vehicle | 11К65М |
| Main experimental results | Electronic surveillance. The Tselina-O spacecraft was upgraded. New instrumentation was provided for Tselina-OM and Tselina-OK spacecraft. |
| Orbited on |
30 October 1967 |
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Tselina-D
|
Mass, kg |
1750 |
| Active life, months | 6 |
| Launch vehicle | 8А92M, 11K68 |
| Main experimental results | Close electronic surveillance |
| Orbited on |
18 December 1970 |
3.png)
Tselina-R
|
Mass, kg |
1750 |
| Active life, months | 6 |
| Launch vehicle | 11K68 |
| Main experimental results |
Radio source observation |
| Orbited on |
10 December 1986 |
3.png)
Tselina-2
|
Mass, kg |
3250 |
| Active life, months | 12 |
| Launch vehicle | 8А82К, 11К77 |
| Main experimental results |
Electronic surveillance |
| Orbited on |
28 September 1984 |

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