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

14051

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: 1987-027B

Object number (NORAD): 17590

Object ID (CCSDS): 17590

Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)

Current information (Y/N): Y

RCS size: LARGE

Orbital parameters

Period: 101.614 minutes

Inclination: 71.0041 deg

SMA: 7213.206 km

Apoapsis: 837.855 km

Periapsis: 832.286 km

RAAN: 309.4522 deg

Eccentricy: 0.00038601

Argument of periapsis: 20.6853 deg

Mean anomaly: 339.4426 deg

Mean motion: 14.17131926 rev/day

Mean motion (dot): 0.00000269 rev/day2

B* drag term: 0.00015743037 1/REarth

Two-line elements (TLE)

Creation date: Sept. 4, 2025, 10:13 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Sept. 4, 2025, 4:56 a.m. UTC

TLE line 0: 0 SL-16 R/B

TLE line 1: 1 17590U 87027B 25247.20610078 .00000269 00000-0 15743-3 0 9990

TLE line 2: 2 17590 71.0041 309.4522 0003860 20.6853 339.4426 14.17131926988969

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
DELTA 1 DEB SSO 2025-02-15 20:35:32 0.0001747051 307.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2025-01-04 18:12:49 0.0001087576 718.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2024-08-19 06:01:33 0.0001805722 167.0 (m) DEBRIS
NOAA 16 DEB SSO 2024-08-14 00:33:19 0.00015387 339.0 (m) DEBRIS
THORAD AGENA D DEB SSO 2024-06-30 17:02:09 0.0001692295 86.0 (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 March 18, 1987, 8:30 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: March 18, 1987, 8:30 a.m. UTC

Rocket: Zenit-2

Launch pad: 45/1

Location: Baikonur Cosmodrome, Republic of Kazakhstan

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