SL-16 DEB

Satellite information

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Satellite Type and Status

DEBRISIN ORBIT

Key statistics

Satellite SL-16 DEB at a glance.

Uptime

14565

Days in orbit

Revolutions

≈ 13.8

Per day

Orbit

LEO

Low Earth Orbit

Inclination

71.0

Latest

Satellite identification and parameters

Extended collection of information and parameters for SL-16 DEB.

Object identification

Identified? True

Debris? True

Object name: SL-16 DEB

International designator: 1985-097C

Object number (NORAD): 16389

Object ID (CCSDS): 16389

Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 104.598 minutes

Inclination: 71.0041 deg

SMA: 7353.775 km

Apoapsis: 1114.864 km

Periapsis: 836.416 km

RAAN: 1.2227 deg

Eccentricy: 0.01893229

Argument of periapsis: 225.0687 deg

Mean anomaly: 133.4926 deg

Mean motion: 13.76693435 rev/day

Mean motion (dot): 0.00000178 rev/day2

B* drag term: 0.00019783507 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, 4:37 p.m. UTC

TLE line 0: 0 SL-16 DEB

TLE line 1: 1 16389U 85097C 25249.69244838 .00000178 00000-0 19784-3 0 9990

TLE line 2: 2 16389 71.0041 1.2227 0189323 225.0687 133.4926 13.76693435 2076

Live tracking on map

Real-time ground track for satellite SL-16 DEB.

In-orbit conjunctions

A list of the most updated potential collisions computed for object SL-16 DEB.

Target Orbit TCA Probability of collision Miss distance Type
THORAD AGENA D DEB SSO 2025-01-29 18:39:18 0.0003628004 56.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2024-08-13 12:20:26 0.0001839811 65.0 (m) DEBRIS

Associated space launch

Dynamic simulator of the Tselina-2 ELINT satellite

SL-16 DEB 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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