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

14953

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: 1984-106C

Object number (NORAD): 15335

Object ID (CCSDS): 15335

Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)

Current information (Y/N): Y

RCS size: MEDIUM

Orbital parameters

Period: 101.194 minutes

Inclination: 66.5547 deg

SMA: 7193.311 km

Apoapsis: 820.598 km

Periapsis: 809.753 km

RAAN: 13.2885 deg

Eccentricy: 0.00075377

Argument of periapsis: 34.9696 deg

Mean anomaly: 138.8521 deg

Mean motion: 14.23015221 rev/day

Mean motion (dot): 0.00000218 rev/day²

B* drag term: 0.00013451214 1/R_Earth

Two-line elements (TLE)

Creation date: Sept. 4, 2025, 10:13 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Sept. 4, 2025, 1:51 a.m. UTC

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

TLE line 1: 1 15335U 84106C 25247.07764693 .00000218 00000-0 13451-3 0 9996

TLE line 2: 2 15335 66.5547 13.2885 0007538 34.9696 138.8521 14.23015221123431

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
NOAA 16 DEB	SSO	2024-11-29 03:00:43	0.0001005617	57.0 (m)	DEBRIS
FENGYUN 1C DEB	SSO	2024-10-14 03:29:10	0.0001102363	82.0 (m)	DEBRIS
CZ-6A DEB	LEO	2024-10-10 10:08:32	0.0002543958	662.0 (m)	DEBRIS
THOR ABLESTAR DEB	LEO	2024-08-20 17:08:48	0.0001886043	499.0 (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.

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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