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

11941

Days in orbit

Revolutions

≈ 14.2

Per day

Orbit

LEO

Low Earth Orbit

Inclination

71.1

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: 1992-093KE

Object number (NORAD): 39714

Object ID (CCSDS): 39714

Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 101.08 minutes

Inclination: 71.0822 deg

SMA: 7187.949 km

Apoapsis: 878.136 km

Periapsis: 741.493 km

RAAN: 275.3127 deg

Eccentricy: 0.00950499

Argument of periapsis: 232.8021 deg

Mean anomaly: 126.4404 deg

Mean motion: 14.24607592 rev/day

Mean motion (dot): 0.00000815 rev/day2

B* drag term: 0.00035462637 1/REarth

Two-line elements (TLE)

Creation date: Sept. 3, 2025, 2:21 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Sept. 2, 2025, 7:38 p.m. UTC

TLE line 0: 0 SL-16 DEB

TLE line 1: 1 39714U 92093KE 25245.81823567 .00000815 00000-0 35463-3 0 9993

TLE line 2: 2 39714 71.0822 275.3127 0095050 232.8021 126.4404 14.24607592611672

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
FENGYUN 1C DEB SSO 2025-03-25 06:52:17 0.0001621311 235.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2025-02-13 13:01:02 0.0003475623 127.0 (m) DEBRIS
CZ-6A DEB SSO 2025-01-21 03:40:53 0.0001097369 271.0 (m) DEBRIS
NOAA 16 DEB SSO 2024-11-15 23:35:16 0.000226354 582.0 (m) DEBRIS
NOAA 16 DEB SSO 2024-11-15 21:53:58 0.0006133059 303.0 (m) DEBRIS

Associated space launch

Second generation ELING satellite

SL-16 DEB was lifted into orbit during the mission ‘Zenit-2 | Tselina-2 12’, on board a Zenit-2 space rocket.

The launch took place on Dec. 25, 1992, 5:56 a.m. from 45/1.

For more information about the launch, click the button.

Launch to space Zenit-2 | Tselina-2 12
Zenit-2 | Tselina-2 12

Agency: N/A

Status: Launch Successful

Launch date: Dec. 25, 1992, 5:56 a.m. UTC

Rocket: Zenit-2

Launch pad: 45/1

Location: Baikonur Cosmodrome, Republic of Kazakhstan

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