SL-12 R/B(AUX MOTOR)

Satellite information

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Satellite Type and Status

ROCKET BODYIN ORBIT

Key statistics

Satellite SL-12 R/B(AUX MOTOR) at a glance.

Uptime

14832

Days in orbit

Revolutions

≈ 14.2

Per day

Orbit

LEO

Low Earth Orbit

Inclination

66.6

Latest

Satellite identification and parameters

Extended collection of information and parameters for SL-12 R/B(AUX MOTOR).

Object identification

Identified? True

Debris? False

Object name: SL-12 R/B(AUX MOTOR)

International designator: 1984-106F

Object number (NORAD): 15338

Object ID (CCSDS): 15338

Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)

Current information (Y/N): Y

RCS size: MEDIUM

Orbital parameters

Period: 101.471 minutes

Inclination: 66.5712 deg

SMA: 7206.457 km

Apoapsis: 842.504 km

Periapsis: 814.14 km

RAAN: 234.8323 deg

Eccentricy: 0.0019679

Argument of periapsis: 249.2019 deg

Mean anomaly: 110.6964 deg

Mean motion: 14.19123069 rev/day

Mean motion (dot): 0.00000267 rev/day2

B* drag term: 0.00016772 1/REarth

Two-line elements (TLE)

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

Reference frame: TEME

Reference center: EARTH

Epoch: May 7, 2025, 4:02 p.m. UTC

TLE line 0: 0 SL-12 R/B(AUX MOTOR)

TLE line 1: 1 15338U 84106F 25127.66873507 .00000267 00000-0 16772-3 0 9999

TLE line 2: 2 15338 66.5712 234.8323 0019679 249.2019 110.6964 14.19123069100681

Live tracking on map

Real-time ground track for satellite SL-12 R/B(AUX MOTOR).

In-orbit conjunctions

A list of the most updated potential collisions computed for object SL-12 R/B(AUX MOTOR).

Target Orbit TCA Probability of collision Miss distance Type
FENGYUN 1C DEB SSO 2025-01-01 22:20:54 0.0001601714 478.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2024-12-06 00:42:13 0.0001262796 28.0 (m) DEBRIS

Associated space launch

Second generation ELING satellite

SL-12 R/B(AUX MOTOR) was lifted into orbit during the mission ‘Proton | Tselina-2 1’, on board a Proton space rocket.

The launch took place on Sept. 28, 1984, 2 p.m. from 200/39 (200L).

For more information about the launch, click the button.

Launch to space Proton | Tselina-2 1
Proton | Tselina-2 1

Agency: N/A

Status: Launch Successful

Launch date: Sept. 28, 1984, 2 p.m. UTC

Rocket: Proton

Launch pad: 200/39 (200L)

Location: Baikonur Cosmodrome, Republic of Kazakhstan

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