Orbital elements of EKRAN 2 DEB
| Launched | 19 September 1977 |
| Flight ended | – |
| Launch site | Tyuratam Missile and Space Center, Kazakhstan (Also known as Baikonur Cosmodrome) |
| Owner | Commonwealth of Independent States (former USSR) |
| NORAD ID | 59986 |
| Date fetched |
Epoch osculation |
Inc. [°] |
Ecc. | RA asc node [hr] |
Arg Peri. [°] |
Mean anom [°] |
Mean motion [rev/day] |
Abs. mag |
| Date fetched |
Epoch osculation |
Inc. [°] |
Ecc. | RA asc node [hr] |
Arg Peri. [°] |
Mean anom [°] |
Mean motion [rev/day] |
Abs. mag |
| 2025 Jul 01 17:56 | 2025 Jun 27 20:53:07 | 4.6829 | 0.00405 | 18.4135 | 109.6261 | 279.7379 | 1.00943 | – |
| 2025 Jun 30 17:56 | 2025 Jun 27 20:53:07 | 4.6829 | 0.00405 | 18.4135 | 109.6261 | 279.7379 | 1.00943 | – |
| 2025 Jun 29 17:56 | 2025 Jun 27 20:53:07 | 4.6829 | 0.00405 | 18.4135 | 109.6261 | 279.7379 | 1.00943 | – |
| 2025 Jun 28 17:56 | 2025 Jun 27 20:53:07 | 4.6829 | 0.00405 | 18.4135 | 109.6261 | 279.7379 | 1.00943 | – |