SL-16 R/B

Satellite information

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Satellite Type and Status

ROCKET BODYIN ORBIT

Key statistics

Satellite SL-16 R/B at a glance.

Uptime

14566

Days in orbit

Revolutions

≈ 14.2

Per day

Orbit

LEO

Low Earth Orbit

Inclination

71.0

Latest

Satellite identification and parameters

Extended collection of information and parameters for SL-16 R/B.

Object identification

Identified? True

Debris? False

Object name: SL-16 R/B

International designator: 1985-097B

Object number (NORAD): 16182

Object ID (CCSDS): 16182

Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)

Current information (Y/N): Y

RCS size: LARGE

Orbital parameters

Period: 101.654 minutes

Inclination: 71.0034 deg

SMA: 7215.133 km

Apoapsis: 842.556 km

Periapsis: 831.44 km

RAAN: 167.3231 deg

Eccentricy: 0.00077035

Argument of periapsis: 193.2695 deg

Mean anomaly: 241.421 deg

Mean motion: 14.16564118 rev/day

Mean motion (dot): 0.00000286 rev/day2

B* drag term: 0.00016744692 1/REarth

Two-line elements (TLE)

Creation date: Sept. 7, 2025, 3:09 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Sept. 6, 2025, 11:17 p.m. UTC

TLE line 0: 0 SL-16 R/B

TLE line 1: 1 16182U 85097B 25249.97042543 .00000286 00000-0 16745-3 0 9995

TLE line 2: 2 16182 71.0034 167.3231 0007703 193.2695 241.4210 14.16564118 61211

Live tracking on map

Real-time ground track for satellite SL-16 R/B.

In-orbit conjunctions

A list of the most updated potential collisions computed for object SL-16 R/B.

Target Orbit TCA Probability of collision Miss distance Type
COSMOS 1275 DEB LEO 2025-08-31 09:45:12 0.002164587 33.0 (m) DEBRIS
DMSP 5D-2 F13 DEB SSO 2025-02-10 02:25:35 0.0002073403 53.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2025-01-26 14:00:56 0.0001465609 356.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2024-11-13 10:27:44 0.0001728706 376.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2024-11-12 17:34:35 0.0002613826 219.0 (m) DEBRIS

Associated space launch

Dynamic simulator of the Tselina-2 ELINT satellite

SL-16 R/B was lifted into orbit during the mission ‘Zenit-2 | GVM Tselina-2’, on board a Zenit-2 space rocket.

The launch took place on Oct. 22, 1985, 7 a.m. from 45/1.

For more information about the launch, click the button.

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

Agency: N/A

Status: Launch Successful

Launch date: Oct. 22, 1985, 7 a.m. UTC

Rocket: Zenit-2

Launch pad: 45/1

Location: Baikonur Cosmodrome, Republic of Kazakhstan

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