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

11860

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: 70.9978 deg

SMA: 7214.328 km

Apoapsis: 846.208 km

Periapsis: 826.178 km

RAAN: 112.8365 deg

Eccentricy: 0.0013882

Argument of periapsis: 210.2003 deg

Mean anomaly: 323.1994 deg

Mean motion: 14.16801357 rev/day

Mean motion (dot): 0.00000244 rev/day²

B* drag term: 0.00014576 1/R_Earth

Two-line elements (TLE)

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

Reference frame: TEME

Reference center: EARTH

Epoch: May 7, 2025, 5:34 p.m. UTC

TLE line 0: 0 SL-16 R/B

TLE line 1: 1 22220U 92076B 25127.73246078 .00000244 00000-0 14576-3 0 9992

TLE line 2: 2 22220 70.9978 112.8365 0013882 210.2003 323.1994 14.16801357678497

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
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
CZ-6A DEB	LEO	2024-10-13 09:59:42	0.0004565859	216.0 (m)	DEBRIS
NOAA 16 DEB	SSO	2024-09-27 14:15:35	0.0001186864	842.0 (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.

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

...

Go to the launch

Latest news about this satellite

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

Return to all satellites

Embed the widget

Just copy the snippet below and paste it as HTML in your article, presentation, e-mail, blog post or website.

<iframe src="https://obdh.space/embed/satcat/22220/" width="400" height="720" frameborder="0"></iframe>

Real-time statistics and tracking

The widget will always be up to date. All data, statistics and tracking map are automatically refreshed in real-time. Check the examples below!

Widget preview

Newsletter sign-up

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