SL-6 R/B

Satellite information

Favourite Embed

Satellite Type and Status

ROCKET BODYIN ORBIT

Key statistics

Satellite SL-6 R/B at a glance.

Uptime

10842

Days in orbit

Revolutions

≈ 14.3

Per day

Orbit

SSO

Sun Synchronous Orbit

Inclination

98.7

Latest

Satellite identification and parameters

Extended collection of information and parameters for SL-6 R/B.

Object identification

Identified? True

Debris? False

Object name: SL-6 R/B

International designator: 1995-072C

Object number (NORAD): 23753

Object ID (CCSDS): 23753

Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)

Current information (Y/N): Y

RCS size: LARGE

Orbital parameters

Period: 100.914 minutes

Inclination: 98.744 deg

SMA: 7180.046 km

Apoapsis: 804.326 km

Periapsis: 799.496 km

RAAN: 312.3706 deg

Eccentricy: 0.00033636

Argument of periapsis: 191.283 deg

Mean anomaly: 168.8276 deg

Mean motion: 14.26960487 rev/day

Mean motion (dot): 0.00000127 rev/day2

B* drag term: 0.000070548054 1/REarth

Two-line elements (TLE)

Creation date: Sept. 3, 2025, 2:21 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Sept. 2, 2025, 9:35 p.m. UTC

TLE line 0: 0 SL-6 R/B

TLE line 1: 1 23753U 95072C 25245.89969297 .00000127 00000-0 70548-4 0 9998

TLE line 2: 2 23753 98.7440 312.3706 0003364 191.2830 168.8276 14.26960487544947

Live tracking on map

Real-time ground track for satellite SL-6 R/B.

In-orbit conjunctions

A list of the most updated potential collisions computed for object SL-6 R/B.

Target Orbit TCA Probability of collision Miss distance Type
METEOR 2-8 DEB LEO 2025-08-04 13:03:15 0.0001370716 350.0 (m) DEBRIS
THOR ABLESTAR DEB LEO 2025-06-10 14:09:25 0.0001173755 348.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2025-05-18 14:48:42 0.0001347193 352.0 (m) DEBRIS
CZ-4 DEB SSO 2025-03-24 17:32:36 0.0001494398 553.0 (m) DEBRIS
THOR ABLESTAR DEB LEO 2025-01-19 14:02:35 0.0001107073 436.0 (m) DEBRIS

Associated space launch

IRS 1C and 1D (Indian Remote Sensing Satellite) were the second version of the series of indigenous state-of-art remote sensing satellites. Skipper was an international project initiated by BMDO to measure the bow-shock UV emissions from reentering bodies at different speeds and heights.

SL-6 R/B was lifted into orbit during the mission ‘Molniya-M | IRS-1C & Skipper’, on board a Molniya-M space rocket.

The launch took place on Dec. 28, 1995, 6:45 a.m. from 31/6.

For more information about the launch, click the button.

Launch to space Molniya-M | IRS-1C & Skipper
Molniya-M | IRS-1C & Skipper

Agency: N/A

Status: Launch Successful

Launch date: Dec. 28, 1995, 6:45 a.m. UTC

Rocket: Molniya-M

Launch pad: 31/6

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.