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

14892

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: 101.47 minutes

Inclination: 66.5713 deg

SMA: 7206.385 km

Apoapsis: 840.268 km

Periapsis: 816.232 km

RAAN: 81.3879 deg

Eccentricy: 0.0016677

Argument of periapsis: 222.3697 deg

Mean anomaly: 137.6108 deg

Mean motion: 14.19144239 rev/day

Mean motion (dot): 0.00000121 rev/day2

B* drag term: 0.000098174 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, 1:53 a.m. UTC

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

TLE line 1: 1 15338U 84106F 25187.07916645 .00000121 00000-0 98174-4 0 9997

TLE line 2: 2 15338 66.5713 81.3879 0016677 222.3697 137.6108 14.19144239109110

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

...

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.