SL-12 R/B(AUX MOTOR)

Satellite information

Favourite Embed

Satellite Type and Status

ROCKET BODYIN ORBIT

Key statistics

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

Uptime

14704

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: 101.039 minutes

Inclination: 66.5861 deg

SMA: 7185.99 km

Apoapsis: 824.251 km

Periapsis: 791.458 km

RAAN: 76.978 deg

Eccentricy: 0.00228173

Argument of periapsis: 170.6 deg

Mean anomaly: 293.0041 deg

Mean motion: 14.25190282 rev/day

Mean motion (dot): 0.00000327 rev/day2

B* drag term: 0.00017498614 1/REarth

Two-line elements (TLE)

Creation date: Sept. 1, 2025, 2:20 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Aug. 31, 2025, 10:03 p.m. UTC

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

TLE line 1: 1 15774U 85042F 25243.91877461 .00000327 00000-0 17499-3 0 9997

TLE line 2: 2 15774 66.5861 76.9780 0022817 170.6000 293.0041 14.25190282 91866

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 2025-06-19 05:07:28 0.0003598034 113.0 (m) DEBRIS
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

...

Latest news about this satellite

There are no fresh news available about this satellite. Check back as we update our databases every day.


Newsletter sign-up

Weekly statistics, charts and insights to help you stay on top of the space industry.