SL-12 DEB

Satellite information

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Satellite Type and Status

DEBRISIN ORBIT

Key statistics

Satellite SL-12 DEB at a glance.

Uptime

14648

Days in orbit

Revolutions

≈ 14.5

Per day

Orbit

LEO

Low Earth Orbit

Inclination

66.6

Latest

Satellite identification and parameters

Extended collection of information and parameters for SL-12 DEB.

Object identification

Identified? True

Debris? True

Object name: SL-12 DEB

International designator: 1985-042G

Object number (NORAD): 18764

Object ID (CCSDS): 18764

Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 99.486 minutes

Inclination: 66.5904 deg

SMA: 7112.155 km

Apoapsis: 802.184 km

Periapsis: 665.857 km

RAAN: 237.7808 deg

Eccentricy: 0.0095841

Argument of periapsis: 215.7626 deg

Mean anomaly: 262.9216 deg

Mean motion: 14.47441184 rev/day

Mean motion (dot): 0.00000237 rev/day2

B* drag term: 0.000086448 1/REarth

Two-line elements (TLE)

Creation date: July 6, 2025, 6:05 p.m.

Reference frame: TEME

Reference center: EARTH

Epoch: July 6, 2025, 1:42 p.m. UTC

TLE line 0: 0 SL-12 DEB

TLE line 1: 1 18764U 85042G 25187.57095321 .00000237 00000-0 86448-4 0 9996

TLE line 2: 2 18764 66.5904 237.7808 0095841 215.7626 262.9216 14.47441184953899

Live tracking on map

Real-time ground track for satellite SL-12 DEB.

In-orbit conjunctions

A list of the most updated potential collisions computed for object SL-12 DEB.

Target Orbit TCA Probability of collision Miss distance Type
IRIDIUM 911 LEO 2025-01-01 06:12:08 0.0003695267 416.0 (m) PAYLOAD

Associated space launch

Second generation ELING satellite

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

The launch took place on May 30, 1985, 2:59 p.m. from 200/40.

For more information about the launch, click the button.

Launch to space Proton | Tselina-2 2
Proton | Tselina-2 2

Agency: N/A

Status: Launch Successful

Launch date: May 30, 1985, 2:59 p.m. UTC

Rocket: Proton

Launch pad: 200/40

Location: Baikonur Cosmodrome, Republic of Kazakhstan

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