SL-16 R/B

Satellite information

Favourite Embed

Satellite Type and Status

ROCKET BODYIN ORBIT

Key statistics

Satellite SL-16 R/B at a glance.

Uptime

13931

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: 101.615 minutes

Inclination: 71.0031 deg

SMA: 7213.272 km

Apoapsis: 840.177 km

Periapsis: 830.098 km

RAAN: 200.8047 deg

Eccentricy: 0.0006986

Argument of periapsis: 240.6957 deg

Mean anomaly: 119.3469 deg

Mean motion: 14.17112284 rev/day

Mean motion (dot): -0.0000017 rev/day2

B* drag term: -0.000060718 1/REarth

Two-line elements (TLE)

Creation date: May 8, 2025, 3:01 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: May 7, 2025, 9:57 p.m. UTC

TLE line 0: 0 SL-16 R/B

TLE line 1: 1 17590U 87027B 25127.91469503 -.00000170 00000-0 -60718-4 0 9996

TLE line 2: 2 17590 71.0031 200.8047 0006986 240.6957 119.3469 14.17112284972067

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

...

Latest news about this satellite

There are no fresh news available about this satellite. Check back as we update our databases every day.


Newsletter sign-up

Weekly statistics, charts and insights to help you stay on top of the space industry.