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

14588

Days in orbit

Revolutions

≈ 14.3

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: 1985-042F

Object number (NORAD): 15774

Object ID (CCSDS): 15774

Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)

Current information (Y/N): Y

RCS size: MEDIUM

Orbital parameters

Period: 101.043 minutes

Inclination: 66.5887 deg

SMA: 7186.172 km

Apoapsis: 830.638 km

Periapsis: 785.436 km

RAAN: 19.2433 deg

Eccentricy: 0.0031451

Argument of periapsis: 242.222 deg

Mean anomaly: 129.0979 deg

Mean motion: 14.25136082 rev/day

Mean motion (dot): 0.00000177 rev/day2

B* drag term: 0.00011108 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, 11:14 p.m. UTC

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

TLE line 1: 1 15774U 85042F 25127.96854740 .00000177 00000-0 11108-3 0 9992

TLE line 2: 2 15774 66.5887 19.2433 0031451 242.2220 129.0979 14.25136082 75344

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 2024-11-29 08:13:00 0.0001122548 442.0 (m) DEBRIS
CZ-6A DEB LEO 2024-09-30 22:30:45 0.0002118899 416.0 (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 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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