Thank you very much for visiting Gunter's Space Page. I hope that this site is useful and informative for you.
If you appreciate the information provided on this site, please consider supporting my work by making a simple and secure donation via PayPal. Please help to run the website and keep everything free of charge. Thank you very much.
EPN 03.0695
EPN 03.0695 [GDK]
The EPN 03.0694 was a dynamic simulator of the Tselina-2 ELINT satellite with additional ballast segments to evaluate the Zenit-2 launch vehicle for heavy payloads.
| Nation: | USSR |
|---|---|
| Type / Application: | Vehicle Evaluation |
| Operator: | |
| Contractors: | |
| Equipment: | |
| Configuration: | |
| Propulsion: | None |
| Power: | |
| Lifetime: | |
| Mass: | |
| Orbit: | 180 km × 190 km, 64.88° (#1767); 171 km × 225 km, 64.83° (#1820); 171 km × 191 km, 97.02° (#1871); 172 km × 229 km, 64.82° (#1873) |
| Satellite | COSPAR | Date | LS | Launch Vehicle | Remarks | |
|---|---|---|---|---|---|---|
| Kosmos 1767 (EPN 03.0695 #1) | 1986-056A | 30.07.1986 | Ba LC-45/1 | Zenit-2 | ||
| Kosmos 1820 (EPN 03.0695 #2) | 1987-016A | 14.02.1987 | Ba LC-45/1 | Zenit-2 | ||
| Kosmos 1871 (EPN 03.0695 #3) | 1987-065A | 01.08.1987 | Ba LC-45/1 | Zenit-2 | ||
| Kosmos 1873 (EPN 03.0695 #4) | 1987-071A | 28.08.1987 | Ba LC-45/1 | Zenit-2 |
Further EPN missions:
