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 | 59988 |
| 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 Sep 25 17:56 | 2025 Sep 09 21:40:27 | 4.6608 | 0.00344 | 18.3710 | 57.0172 | 2.1036 | 1.00849 | – |
| 2025 Sep 24 17:56 | 2025 Sep 09 21:40:27 | 4.6608 | 0.00344 | 18.3710 | 57.0172 | 2.1036 | 1.00849 | – |
| 2025 Sep 20 17:56 | 2025 Sep 09 21:40:27 | 4.6608 | 0.00344 | 18.3710 | 57.0172 | 2.1036 | 1.00849 | – |
| 2025 Sep 19 17:56 | 2025 Sep 09 21:40:27 | 4.6608 | 0.00344 | 18.3710 | 57.0172 | 2.1036 | 1.00849 | – |
| 2025 Sep 18 17:56 | 2025 Sep 09 21:40:27 | 4.6608 | 0.00344 | 18.3710 | 57.0172 | 2.1036 | 1.00849 | – |