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

11920

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: 1992-076B

Object number (NORAD): 22220

Object ID (CCSDS): 22220

Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)

Current information (Y/N): Y

RCS size: LARGE

Orbital parameters

Period: 101.637 minutes

Inclination: 71.0009 deg

SMA: 7214.306 km

Apoapsis: 843.995 km

Periapsis: 828.348 km

RAAN: 346.7733 deg

Eccentricy: 0.0010844

Argument of periapsis: 114.4094 deg

Mean anomaly: 314.2102 deg

Mean motion: 14.16807608 rev/day

Mean motion (dot): -0.00000058 rev/day2

B* drag term: -0.0000051848 1/REarth

Two-line elements (TLE)

Creation date: July 6, 2025, 2:46 p.m.

Reference frame: TEME

Reference center: EARTH

Epoch: July 6, 2025, 1:59 p.m. UTC

TLE line 0: 0 SL-16 R/B

TLE line 1: 1 22220U 92076B 25187.58277826 -.00000058 00000-0 -51848-5 0 9996

TLE line 2: 2 22220 71.0009 346.7733 0010844 114.4094 314.2102 14.16807608687308

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
FENGYUN 1C DEB SSO 2025-06-30 03:01:10 0.0005681265 24.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2025-05-26 00:17:13 0.0001132795 253.0 (m) DEBRIS
CZ-6A DEB SSO 2025-05-08 03:59:36 0.0001829047 398.0 (m) DEBRIS
DELTA 1 DEB SSO 2025-04-08 09:40:06 0.0001117206 625.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2024-11-14 04:53:18 0.0001016493 210.0 (m) DEBRIS

Associated space launch

Second generation ELING satellite

SL-16 R/B was lifted into orbit during the mission ‘Zenit-2 | Tselina-2 11’, on board a Zenit-2 space rocket.

The launch took place on Nov. 17, 1992, 7:47 a.m. from 45/1.

For more information about the launch, click the button.

Launch to space Zenit-2 | Tselina-2 11
Zenit-2 | Tselina-2 11

Agency: N/A

Status: Launch Successful

Launch date: Nov. 17, 1992, 7:47 a.m. UTC

Rocket: Zenit-2

Launch pad: 45/1

Location: Baikonur Cosmodrome, Republic of Kazakhstan

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