COSMOS 2082

Satellite information

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Satellite Type and Status

PAYLOADIN ORBIT

Key statistics

Satellite COSMOS 2082 at a glance.

Uptime

12933

Days in orbit

Revolutions

≈ 14.1

Per day

Orbit

LEO

Low Earth Orbit

Inclination

71.0

Latest

Satellite identification and parameters

Extended collection of information and parameters for COSMOS 2082.

Object identification

Identified? True

Debris? False

Object name: COSMOS 2082

International designator: 1990-046A

Object number (NORAD): 20624

Object ID (CCSDS): 20624

Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)

Current information (Y/N): Y

RCS size: LARGE

Orbital parameters

Period: 101.782 minutes

Inclination: 71.0397 deg

SMA: 7221.158 km

Apoapsis: 852.279 km

Periapsis: 833.767 km

RAAN: 320.1092 deg

Eccentricy: 0.00128179

Argument of periapsis: 57.7605 deg

Mean anomaly: 302.4759 deg

Mean motion: 14.1479163 rev/day

Mean motion (dot): 0.00000067 rev/day2

B* drag term: 0.000058995327 1/REarth

Two-line elements (TLE)

Creation date: Oct. 18, 2025, 2:17 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Oct. 17, 2025, 6:45 p.m. UTC

TLE line 0: 0 COSMOS 2082

TLE line 1: 1 20624U 90046A 25290.78140390 .00000067 00000-0 58995-4 0 9996

TLE line 2: 2 20624 71.0397 320.1092 0012818 57.7605 302.4759 14.14791630827418

Live tracking on map

Real-time ground track for satellite COSMOS 2082.

In-orbit conjunctions

A list of the most updated potential collisions computed for object COSMOS 2082.

Target Orbit TCA Probability of collision Miss distance Type
CZ-6A DEB LEO 2025-04-07 12:49:26 0.0002626742 71.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2025-03-25 20:06:18 0.0001482902 180.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2024-12-11 22:26:13 0.0001293994 460.0 (m) DEBRIS
SL-16 DEB LEO 2024-12-10 01:34:45 0.0001616514 171.0 (m) DEBRIS
DELTA 1 DEB SSO 2024-10-31 20:09:54 0.0001202493 82.0 (m) DEBRIS

Associated space launch

Second generation ELING satellite

COSMOS 2082 was lifted into orbit during the mission ‘Zenit-2 | Tselina-2 7’, on board a Zenit-2 space rocket.

The launch took place on May 22, 1990, 5:14 a.m. from 45/2.

For more information about the launch, click the button.

Launch to space Zenit-2 | Tselina-2 7
Zenit-2 | Tselina-2 7

Agency: N/A

Status: Launch Successful

Launch date: May 22, 1990, 5:14 a.m. UTC

Rocket: Zenit-2

Launch pad: 45/2

Location: Baikonur Cosmodrome, Republic of Kazakhstan

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